Meteor impact events such as Chelyabinsk are known to cause catastrophic impacts every few hundred years. The modern-day fallout from such event can cause large loss of life and property. One satellite in Low Earth Orbit (LEO) may get a glimpse of a meteor trail. However, a swarm constellation has the potential of performing persistent, realtime global tracking of an incoming meteor. Developing a swarm constellation using a fleet of large satellites is an expensive endeavor. A cost-effective alternative is to use CubeSats and small-satellites that contain the latest, onboard computers, sensors and communication devices for low-mass and low-volume. Our inspiration for a swarm constellation comes from eusocial insects that are composed of simple individuals, that are decentralized, that operate autonomously using only local sensing and are robust to individual losses. This work illustrates the design of a constellation of large number CubeSats in LEO at altitude of 400 km and higher, referred to as a swarm, in order to monitor the skies above entire North America. Specifically, this work extends the capability of a 3U CubeSat mission known as SWIMSat, by converting it into a swarm, to monitor the region over North America at an altitude of 140 km. The design of a swarm in LEO faces multiple challenges such as the limited field of view of the spacecraft-instrument and resulting observation quality. The design is further complicated by the fact that in order to enable triangulation of the meteor event, the entire region of interest should be observed by at least two nodes. Due to the complicated nature of the problem, an analytical treatment is challenging. This work aims to solve these challenges by the reducing the problem into designing a circular Walker-Delta constellation in LEO, with repeating ground track orbits. The approach employed in the work is as follows: First, an optimal orbit inclination is determined by propagating the orbit forward in time. Here a cost
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