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 68221U 26145.38819412 +.00000000 +00000-0 +39383-3 0 00005
2 68221 97.2873 20.8545 0001739 92.8763 267.2678 15.33451473 00
| Epoch (UTC): | 25 May 2026 09:18:59 |
| Eccentricity: | 0.0001739 |
| inclination: | 97.2873° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 20.8545° |
| argument of perigee: | 92.8763° |
| revolutions per day: | 15.33451473 |
| mean anomaly at epoch: | 267.2678° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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