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 26150.50045006 +.00000000 +00000-0 +11231-3 0 00007
2 25994 97.9466 200.7469 0000873 303.9967 193.3751 14.61087297 09
| Epoch (UTC): | 30 May 2026 12:00:38 |
| Eccentricity: | 0.0000873 |
| inclination: | 97.9466° |
| perigee height: | 689 km |
| apogee height: | 690 km |
| right ascension of ascending node: | 200.7469° |
| argument of perigee: | 303.9967° |
| revolutions per day: | 14.61087297 |
| mean anomaly at epoch: | 193.3751° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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