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 20U 59007A 25318.35490720 .00004072 00000-0 16295-2 0 9990
2 20 33.3473 320.2845 1639842 342.0680 12.8071 11.61459710459627
| Epoch (UTC): | 14 November 2025 08:31:03 |
| Eccentricity: | 0.1639842 |
| inclination: | 33.3473° |
| perigee height: | 507 km |
| apogee height: | 3209 km |
| right ascension of ascending node: | 320.2845° |
| argument of perigee: | 342.0680° |
| revolutions per day: | 11.61459710 |
| mean anomaly at epoch: | 12.8071° |
| orbit number at epoch: | 45962 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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