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 68321U 26144.80748204 +.00000000 +00000-0 +63033-3 0 00001
2 68321 53.1571 354.4155 0000694 93.0206 267.0874 15.30207725 06
| Epoch (UTC): | 24 May 2026 19:22:46 |
| Eccentricity: | 0.0000694 |
| inclination: | 53.1571° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 354.4155° |
| argument of perigee: | 93.0206° |
| revolutions per day: | 15.30207725 |
| mean anomaly at epoch: | 267.0874° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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