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 00082U 61004B 25339.33352666 .00000478 00000-0 42915-3 0 9990
2 00082 38.8585 359.8140 1167344 7.5968 354.0843 12.27804881 52971
| Epoch (UTC): | 05 December 2025 08:00:16 |
| Eccentricity: | 0.1167344 |
| inclination: | 38.8585° |
| perigee height: | 632 km |
| apogee height: | 2485 km |
| right ascension of ascending node: | 359.8140° |
| argument of perigee: | 7.5968° |
| revolutions per day: | 12.27804881 |
| mean anomaly at epoch: | 354.0843° |
| orbit number at epoch: | 5297 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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