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 is defined by the following mean orbital elements,
1 58471U 23185K 25114.86339687 .10095164 24939-5 11708-2 0 9994
2 58471 97.3435 194.4543 0015215 263.2900 96.6666 16.36438907 78320
| Epoch (UTC): | 24 April 2025 20:43:17 |
| Eccentricity: | 0.0015215 |
| inclination: | 97.3435° |
| perigee height: | 165 km |
| apogee height: | 185 km |
| right ascension of ascending node: | 194.4543° |
| argument of perigee: | 263.2900° |
| revolutions per day: | 16.36438907 |
| mean anomaly at epoch: | 96.6666° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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