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 38789U 99025EUD 24355.88386172 .00005562 00000-0 12743-2 0 9999
2 38789 98.9025 219.9356 0217132 10.6207 4.2871 14.42528689566948
| Epoch (UTC): | 20 December 2024 21:12:45 |
| Eccentricity: | 0.0217132 |
| inclination: | 98.9025° |
| perigee height: | 595 km |
| apogee height: | 905 km |
| right ascension of ascending node: | 219.9356° |
| argument of perigee: | 10.6207° |
| revolutions per day: | 14.42528689 |
| mean anomaly at epoch: | 4.2871° |
| orbit number at epoch: | 56694 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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