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 05118U 71028B 25197.90047636 .00012676 00000-0 25542-3 0 9995
2 05118 81.2435 339.4314 0024113 42.6525 317.6586 15.46097467952081
| Epoch (UTC): | 16 July 2025 21:36:41 |
| Eccentricity: | 0.0024113 |
| inclination: | 81.2435° |
| perigee height: | 412 km |
| apogee height: | 444 km |
| right ascension of ascending node: | 339.4314° |
| argument of perigee: | 42.6525° |
| revolutions per day: | 15.46097467 |
| mean anomaly at epoch: | 317.6586° |
| orbit number at epoch: | 95208 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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