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 25397U 26037.90281676 +.00000000 +00000-0 +79038-4 0 00007
2 25397 98.9987 27.4306 0000773 178.6118 181.5062 14.24397158 06
| Epoch (UTC): | 06 February 2026 21:40:03 |
| Eccentricity: | 0.0000773 |
| inclination: | 98.9987° |
| perigee height: | 810 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 27.4306° |
| argument of perigee: | 178.6118° |
| revolutions per day: | 14.24397158 |
| mean anomaly at epoch: | 181.5062° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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