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 25544U 26045.79523799 +.00000000 +00000-0 +15107-3 0 00008
2 25544 51.6315 185.5279 0011056 98.8248 261.3993 15.48601910 00
| Epoch (UTC): | 14 February 2026 19:05:08 |
| Eccentricity: | 0.0011056 |
| inclination: | 51.6315° |
| perigee height: | 413 km |
| apogee height: | 428 km |
| right ascension of ascending node: | 185.5279° |
| argument of perigee: | 98.8248° |
| revolutions per day: | 15.48601910 |
| mean anomaly at epoch: | 261.3993° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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