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 10061U 77048A 25197.77058543 -.00000269 00000-0 00000-0 0 9995
2 10061 7.2177 296.1342 0011068 49.4044 348.1960 0.99398335 42941
| Epoch (UTC): | 16 July 2025 18:29:38 |
| Eccentricity: | 0.0011068 |
| inclination: | 7.2177° |
| perigee height: | 35986 km |
| apogee height: | 36080 km |
| right ascension of ascending node: | 296.1342° |
| argument of perigee: | 49.4044° |
| revolutions per day: | 0.99398335 |
| mean anomaly at epoch: | 348.1960° |
| orbit number at epoch: | 4294 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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