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 60969U 26088.02182372 +.00000000 +00000-0 +10882-3 0 00004
2 60969 89.0008 284.3875 0053760 104.2509 256.4659 14.18186820 02
| Epoch (UTC): | 29 March 2026 00:31:25 |
| Eccentricity: | 0.0053760 |
| inclination: | 89.0008° |
| perigee height: | 793 km |
| apogee height: | 870 km |
| right ascension of ascending node: | 284.3875° |
| argument of perigee: | 104.2509° |
| revolutions per day: | 14.18186820 |
| mean anomaly at epoch: | 256.4659° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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