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 26121.50800983 +.00000000 +00000-0 +44443-3 0 00001
2 25112 45.0139 278.1582 0005608 78.5001 281.6481 14.47145143 02
| Epoch (UTC): | 01 May 2026 12:11:32 |
| Eccentricity: | 0.0005608 |
| inclination: | 45.0139° |
| perigee height: | 731 km |
| apogee height: | 739 km |
| right ascension of ascending node: | 278.1582° |
| argument of perigee: | 78.5001° |
| revolutions per day: | 14.47145143 |
| mean anomaly at epoch: | 281.6481° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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