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 25396U 26038.90939332 +.00000000 +00000-0 +11173-3 0 00001
2 25396 98.9774 26.8169 0002879 154.8908 205.2411 14.25710426 01
| Epoch (UTC): | 07 February 2026 21:49:31 |
| Eccentricity: | 0.0002879 |
| inclination: | 98.9774° |
| perigee height: | 804 km |
| apogee height: | 808 km |
| right ascension of ascending node: | 26.8169° |
| argument of perigee: | 154.8908° |
| revolutions per day: | 14.25710426 |
| mean anomaly at epoch: | 205.2411° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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