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 25349.90600187 .00000462 00000-0 10357-3 0 9996
2 25994 97.9746 41.4743 0003602 88.3629 84.4744 14.60905450382843
| Epoch (UTC): | 15 December 2025 21:44:38 |
| Eccentricity: | 0.0003602 |
| inclination: | 97.9746° |
| perigee height: | 688 km |
| apogee height: | 693 km |
| right ascension of ascending node: | 41.4743° |
| argument of perigee: | 88.3629° |
| revolutions per day: | 14.60905450 |
| mean anomaly at epoch: | 84.4744° |
| orbit number at epoch: | 38284 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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