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 55402U 26145.52907337 +.00000000 +00000-0 +24678-4 0 00004
2 55402 69.9992 230.7766 0003086 266.1498 93.9308 14.98331040 01
| Epoch (UTC): | 25 May 2026 12:41:51 |
| Eccentricity: | 0.0003086 |
| inclination: | 69.9992° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 230.7766° |
| argument of perigee: | 266.1498° |
| revolutions per day: | 14.98331040 |
| mean anomaly at epoch: | 93.9308° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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