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 22830U 93061H 25191.44048532 .00000125 00000-0 61961-4 0 9997
2 22830 98.5261 259.6361 0009497 282.1320 77.8799 14.32674552659418
| Epoch (UTC): | 10 July 2025 10:34:17 |
| Eccentricity: | 0.0009497 |
| inclination: | 98.5261° |
| perigee height: | 776 km |
| apogee height: | 789 km |
| right ascension of ascending node: | 259.6361° |
| argument of perigee: | 282.1320° |
| revolutions per day: | 14.32674552 |
| mean anomaly at epoch: | 77.8799° |
| orbit number at epoch: | 65941 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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