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 61760U 24199AB 25322.52137139 .00038202 00000-0 81734-3 0 9991
2 61760 97.3249 191.9239 0007201 343.1339 16.9669 15.44682785105032
| Epoch (UTC): | 18 November 2025 12:30:46 |
| Eccentricity: | 0.0007201 |
| inclination: | 97.3249° |
| perigee height: | 427 km |
| apogee height: | 437 km |
| right ascension of ascending node: | 191.9239° |
| argument of perigee: | 343.1339° |
| revolutions per day: | 15.44682785 |
| mean anomaly at epoch: | 16.9669° |
| orbit number at epoch: | 10503 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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