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 68211U 26145.60842565 +.00000000 +00000-0 +78260-4 0 00002
2 68211 97.2868 21.0145 0002116 92.8309 267.3176 15.33462838 09
| Epoch (UTC): | 25 May 2026 14:36:07 |
| Eccentricity: | 0.0002116 |
| inclination: | 97.2868° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 21.0145° |
| argument of perigee: | 92.8309° |
| revolutions per day: | 15.33462838 |
| mean anomaly at epoch: | 267.3176° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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