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 data is extracted from the following two-line orbital elements,
1 00107U 61013A 23337.09884741 .00003972 00000-0 49933-3 0 9990
2 00107 28.7859 230.1057 0527444 161.6274 200.4138 14.13745637144761
| Epoch (UTC): | 03 December 2023 02:22:20 |
| Eccentricity: | 0.0527444 |
| inclination: | 28.7859° |
| perigee height: | 465 km |
| apogee height: | 1227 km |
| right ascension of ascending node: | 230.1057° |
| argument of perigee: | 161.6274° |
| revolutions per day: | 14.13745637 |
| mean anomaly at epoch: | 200.4138° |
| orbit number at epoch: | 14476 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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