View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 53378U 22096J 24228.06623961 .01972063 41844-2 15090-2 0 9994
2 53378 97.3908 151.6448 0008407 161.8615 198.2973 16.16088910113554
| Epoch (UTC): | 15 August 2024 01:35:23 |
| Eccentricity: | 0.0008407 |
| inclination: | 97.3908° |
| perigee height: | 224 km |
| apogee height: | 236 km |
| right ascension of ascending node: | 151.6448° |
| argument of perigee: | 161.8615° |
| revolutions per day: | 16.16088910 |
| mean anomaly at epoch: | 198.2973° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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