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 26037.53476766 +.00000000 +00000-0 +22585-3 0 00000
2 25544 51.6316 226.3678 0011133 70.9201 289.2992 15.48439420 07
| Epoch (UTC): | 06 February 2026 12:50:03 |
| Eccentricity: | 0.0011133 |
| inclination: | 51.6316° |
| perigee height: | 414 km |
| apogee height: | 429 km |
| right ascension of ascending node: | 226.3678° |
| argument of perigee: | 70.9201° |
| revolutions per day: | 15.48439420 |
| mean anomaly at epoch: | 289.2992° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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