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 21422U 91042A 25189.51341754 .00001501 00000-0 12181-3 0 9995
2 21422 82.4984 318.9221 0013101 158.6731 201.5041 14.98911031847752
| Epoch (UTC): | 08 July 2025 12:19:19 |
| Eccentricity: | 0.0013101 |
| inclination: | 82.4984° |
| perigee height: | 561 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 318.9221° |
| argument of perigee: | 158.6731° |
| revolutions per day: | 14.98911031 |
| mean anomaly at epoch: | 201.5041° |
| orbit number at epoch: | 84775 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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