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 25394U 26032.49937081 +.00000000 +00000-0 +89071-4 0 00009
2 25394 98.9261 3.6016 0001971 130.9901 229.1448 14.25071363 09
| Epoch (UTC): | 01 February 2026 11:59:05 |
| Eccentricity: | 0.0001971 |
| inclination: | 98.9261° |
| perigee height: | 807 km |
| apogee height: | 810 km |
| right ascension of ascending node: | 3.6016° |
| argument of perigee: | 130.9901° |
| revolutions per day: | 14.25071363 |
| mean anomaly at epoch: | 229.1448° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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