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 68210U 26145.21961664 +.00000000 +00000-0 +43513-3 0 00002
2 68210 97.2858 20.6246 0001421 92.6530 267.4875 15.33454412 02
| Epoch (UTC): | 25 May 2026 05:16:14 |
| Eccentricity: | 0.0001421 |
| inclination: | 97.2858° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 20.6246° |
| argument of perigee: | 92.6530° |
| revolutions per day: | 15.33454412 |
| mean anomaly at epoch: | 267.4875° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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