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 25350.99188867 .00000442 00000-0 99486-4 0 9992
2 25994 97.9744 42.5202 0003586 86.1451 34.2468 14.60906801383009
| Epoch (UTC): | 16 December 2025 23:48:19 |
| Eccentricity: | 0.0003586 |
| inclination: | 97.9744° |
| perigee height: | 688 km |
| apogee height: | 693 km |
| right ascension of ascending node: | 42.5202° |
| argument of perigee: | 86.1451° |
| revolutions per day: | 14.60906801 |
| mean anomaly at epoch: | 34.2468° |
| orbit number at epoch: | 38300 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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