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 26038.95648498 +.00000000 +00000-0 +69417-4 0 00002
2 25397 98.9989 28.5095 0000836 175.4729 184.6457 14.24397369 04
| Epoch (UTC): | 07 February 2026 22:57:20 |
| Eccentricity: | 0.0000836 |
| inclination: | 98.9989° |
| perigee height: | 810 km |
| apogee height: | 811 km |
| right ascension of ascending node: | 28.5095° |
| argument of perigee: | 175.4729° |
| revolutions per day: | 14.24397369 |
| mean anomaly at epoch: | 184.6457° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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