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 25994U 99068A 25191.60429341 .00000273 00000-0 65108-4 0 9994
2 25994 97.9969 248.7702 0001622 189.6650 295.4105 14.60729223359735
| Epoch (UTC): | 10 July 2025 14:30:10 |
| Eccentricity: | 0.0001622 |
| inclination: | 97.9969° |
| perigee height: | 689 km |
| apogee height: | 692 km |
| right ascension of ascending node: | 248.7702° |
| argument of perigee: | 189.6650° |
| revolutions per day: | 14.60729223 |
| mean anomaly at epoch: | 295.4105° |
| orbit number at epoch: | 35973 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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