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 68522U 26145.25073205 +.00000000 +00000-0 +89876-3 0 00009
2 68522 53.1587 132.4473 0001307 87.3660 272.7493 15.34407881 04
| Epoch (UTC): | 25 May 2026 06:01:03 |
| Eccentricity: | 0.0001307 |
| inclination: | 53.1587° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 132.4473° |
| argument of perigee: | 87.3660° |
| revolutions per day: | 15.34407881 |
| mean anomaly at epoch: | 272.7493° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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