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 is defined by the following mean orbital elements,
1 25994U 26017.96414367 +.00000000 +00000-0 +92955-4 0 00002
2 25994 97.9695 73.3100 0002157 16.0920 36.8161 14.60947242 07
| Epoch (UTC): | 17 January 2026 23:08:22 |
| Eccentricity: | 0.0002157 |
| inclination: | 97.9695° |
| perigee height: | 689 km |
| apogee height: | 692 km |
| right ascension of ascending node: | 73.3100° |
| argument of perigee: | 16.0920° |
| revolutions per day: | 14.60947242 |
| mean anomaly at epoch: | 36.8161° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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