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 25979U 26070.20459730 +.00000000 +00000-0 +72462-3 0 00004
2 25979 98.1628 152.4695 0004919 86.8572 273.3230 15.31433719 06
| Epoch (UTC): | 11 March 2026 04:54:37 |
| Eccentricity: | 0.0004919 |
| inclination: | 98.1628° |
| perigee height: | 468 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 152.4695° |
| argument of perigee: | 86.8572° |
| revolutions per day: | 15.31433719 |
| mean anomaly at epoch: | 273.3230° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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