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 25118.46921391 .00007903 00000-0 96491-3 0 9992
2 00107 28.7880 182.7654 0505492 222.9528 133.0498 14.19377590217465
| Epoch (UTC): | 28 April 2025 11:15:40 |
| Eccentricity: | 0.0505492 |
| inclination: | 28.7880° |
| perigee height: | 463 km |
| apogee height: | 1191 km |
| right ascension of ascending node: | 182.7654° |
| argument of perigee: | 222.9528° |
| revolutions per day: | 14.19377590 |
| mean anomaly at epoch: | 133.0498° |
| orbit number at epoch: | 21746 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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