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 37391U 11014B 25136.08590652 0.00000000 00000-0 00000-0 0 05
2 37391 63.4346 215.1442 0319026 357.3620 2.6380 13.40968020 09
| Epoch (UTC): | 16 May 2025 02:03:42 |
| Eccentricity: | 0.0319026 |
| inclination: | 63.4346° |
| perigee height: | 867 km |
| apogee height: | 1344 km |
| right ascension of ascending node: | 215.1442° |
| argument of perigee: | 357.3620° |
| revolutions per day: | 13.40968020 |
| mean anomaly at epoch: | 2.6380° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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