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 25261U 98017B 25162.65155461 .00000277 00000-0 11145-3 0 9991
2 25261 98.8431 179.4094 0004393 126.1989 233.9603 14.35965911422806
| Epoch (UTC): | 11 June 2025 15:38:14 |
| Eccentricity: | 0.0004393 |
| inclination: | 98.8431° |
| perigee height: | 769 km |
| apogee height: | 775 km |
| right ascension of ascending node: | 179.4094° |
| argument of perigee: | 126.1989° |
| revolutions per day: | 14.35965911 |
| mean anomaly at epoch: | 233.9603° |
| orbit number at epoch: | 42280 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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