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 21610U 91050F 25191.57245794 .00000193 00000-0 70649-4 0 9999
2 21610 98.2382 247.3996 0004457 90.3053 269.8648 14.42651694784086
| Epoch (UTC): | 10 July 2025 13:44:20 |
| Eccentricity: | 0.0004457 |
| inclination: | 98.2382° |
| perigee height: | 746 km |
| apogee height: | 753 km |
| right ascension of ascending node: | 247.3996° |
| argument of perigee: | 90.3053° |
| revolutions per day: | 14.42651694 |
| mean anomaly at epoch: | 269.8648° |
| orbit number at epoch: | 78408 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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