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 26070.14813214 +.00000000 +00000-0 +10913-3 0 00009
2 06257 81.2604 318.2934 0056462 153.0784 207.3335 14.06873053 04
| Epoch (UTC): | 11 March 2026 03:33:18 |
| Eccentricity: | 0.0056462 |
| inclination: | 81.2604° |
| perigee height: | 829 km |
| apogee height: | 911 km |
| right ascension of ascending node: | 318.2934° |
| argument of perigee: | 153.0784° |
| revolutions per day: | 14.06873053 |
| mean anomaly at epoch: | 207.3335° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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