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 37168U 10048A 25141.88884667 .00003989 00000-0 21159-3 0 9996
2 37168 97.7886 14.5739 0089415 108.1322 22.5598 15.12529858793315
| Epoch (UTC): | 21 May 2025 21:19:56 |
| Eccentricity: | 0.0089415 |
| inclination: | 97.7886° |
| perigee height: | 467 km |
| apogee height: | 590 km |
| right ascension of ascending node: | 14.5739° |
| argument of perigee: | 108.1322° |
| revolutions per day: | 15.12529858 |
| mean anomaly at epoch: | 22.5598° |
| orbit number at epoch: | 79331 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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