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 00058U 60013A 25082.83409379 .00000155 00000-0 10958-3 0 9990
2 00058 28.3268 264.8631 0164769 78.6421 283.2586 13.46405689173321
| Epoch (UTC): | 23 March 2025 20:01:05 |
| Eccentricity: | 0.0164769 |
| inclination: | 28.3268° |
| perigee height: | 962 km |
| apogee height: | 1208 km |
| right ascension of ascending node: | 264.8631° |
| argument of perigee: | 78.6421° |
| revolutions per day: | 13.46405689 |
| mean anomaly at epoch: | 283.2586° |
| orbit number at epoch: | 17332 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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