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 21088U 91006B 25191.52440515 .00000090 00000-0 75603-4 0 9993
2 21088 82.9434 350.1914 0022322 357.1450 65.3211 13.77463182730730
| Epoch (UTC): | 10 July 2025 12:35:08 |
| Eccentricity: | 0.0022322 |
| inclination: | 82.9434° |
| perigee height: | 956 km |
| apogee height: | 989 km |
| right ascension of ascending node: | 350.1914° |
| argument of perigee: | 357.1450° |
| revolutions per day: | 13.77463182 |
| mean anomaly at epoch: | 65.3211° |
| orbit number at epoch: | 73073 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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