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 26145.64088029 +.00000000 +00000-0 +75570-4 0 00005
2 25994 97.9470 196.0795 0001152 334.3287 177.4537 14.61081907 04
| Epoch (UTC): | 25 May 2026 15:22:52 |
| Eccentricity: | 0.0001152 |
| inclination: | 97.9470° |
| perigee height: | 689 km |
| apogee height: | 690 km |
| right ascension of ascending node: | 196.0795° |
| argument of perigee: | 334.3287° |
| revolutions per day: | 14.61081907 |
| mean anomaly at epoch: | 177.4537° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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