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 107U 61013A 23088.99816781 .00003297 00000-0 41995-3 0 9991
2 107 28.7856 199.3108 0535913 39.2456 324.5742 14.11692937109204
| Epoch (UTC): | 29 March 2023 23:57:21 |
| Eccentricity: | 0.0535913 |
| inclination: | 28.7856° |
| perigee height: | 466 km |
| apogee height: | 1241 km |
| right ascension of ascending node: | 199.3108° |
| argument of perigee: | 39.2456° |
| revolutions per day: | 14.11692937 |
| mean anomaly at epoch: | 324.5742° |
| orbit number at epoch: | 10920 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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