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 25112U 26065.51821227 +.00000000 +00000-0 +75756-3 0 00004
2 25112 45.0125 187.4789 0006874 155.3336 204.7846 14.46967295 09
| Epoch (UTC): | 06 March 2026 12:26:13 |
| Eccentricity: | 0.0006874 |
| inclination: | 45.0125° |
| perigee height: | 731 km |
| apogee height: | 740 km |
| right ascension of ascending node: | 187.4789° |
| argument of perigee: | 155.3336° |
| revolutions per day: | 14.46967295 |
| mean anomaly at epoch: | 204.7846° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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