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 25082.52636336 .00005946 00000-0 72225-3 0 9995
2 00107 28.7927 29.0229 0507496 248.8989 105.6615 14.18928984212359
| Epoch (UTC): | 23 March 2025 12:37:57 |
| Eccentricity: | 0.0507496 |
| inclination: | 28.7927° |
| perigee height: | 463 km |
| apogee height: | 1195 km |
| right ascension of ascending node: | 29.0229° |
| argument of perigee: | 248.8989° |
| revolutions per day: | 14.18928984 |
| mean anomaly at epoch: | 105.6615° |
| orbit number at epoch: | 21235 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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