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 06257U 26100.01815838 +.00000000 +00000-0 -45733-4 0 00003
2 06257 81.2560 289.4125 0058216 69.9625 290.7799 14.06877819 08
| Epoch (UTC): | 10 April 2026 00:26:08 |
| Eccentricity: | 0.0058216 |
| inclination: | 81.2560° |
| perigee height: | 828 km |
| apogee height: | 912 km |
| right ascension of ascending node: | 289.4125° |
| argument of perigee: | 69.9625° |
| revolutions per day: | 14.06877819 |
| mean anomaly at epoch: | 290.7799° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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