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 68021U 26145.37284661 +.00000000 +00000-0 +61739-3 0 00004
2 68021 97.2854 94.3686 0002432 113.2007 246.9492 15.33451471 05
| Epoch (UTC): | 25 May 2026 08:56:53 |
| Eccentricity: | 0.0002432 |
| inclination: | 97.2854° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 94.3686° |
| argument of perigee: | 113.2007° |
| revolutions per day: | 15.33451471 |
| mean anomaly at epoch: | 246.9492° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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