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 07210U 74011B 25346.23593359 .00000154 00000-0 72948-4 0 9996
2 07210 81.2362 251.4129 0079963 199.5916 160.2181 14.13603107667578
| Epoch (UTC): | 12 December 2025 05:39:44 |
| Eccentricity: | 0.0079963 |
| inclination: | 81.2362° |
| perigee height: | 789 km |
| apogee height: | 905 km |
| right ascension of ascending node: | 251.4129° |
| argument of perigee: | 199.5916° |
| revolutions per day: | 14.13603107 |
| mean anomaly at epoch: | 160.2181° |
| orbit number at epoch: | 66757 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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