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 00059U 60013B 25347.74892594 .00000130 00000-0 51712-4 0 9997
2 00059 28.2507 356.3752 0188879 198.8969 160.4489 13.53154955218039
| Epoch (UTC): | 13 December 2025 17:58:27 |
| Eccentricity: | 0.0188879 |
| inclination: | 28.2507° |
| perigee height: | 920 km |
| apogee height: | 1201 km |
| right ascension of ascending node: | 356.3752° |
| argument of perigee: | 198.8969° |
| revolutions per day: | 13.53154955 |
| mean anomaly at epoch: | 160.4489° |
| orbit number at epoch: | 21803 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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