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 26037.98653626 +.00000000 +00000-0 +22894-3 0 00004
2 25544 51.6315 224.1327 0011143 71.6186 288.6013 15.48450046 08
| Epoch (UTC): | 06 February 2026 23:40:36 |
| Eccentricity: | 0.0011143 |
| inclination: | 51.6315° |
| perigee height: | 414 km |
| apogee height: | 429 km |
| right ascension of ascending node: | 224.1327° |
| argument of perigee: | 71.6186° |
| revolutions per day: | 15.48450046 |
| mean anomaly at epoch: | 288.6013° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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