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 68502U 26145.38339517 +.00000000 +00000-0 +90213-4 0 00000
2 68502 97.7613 103.9926 0003643 88.2498 271.9137 14.91639320 09
| Epoch (UTC): | 25 May 2026 09:12:05 |
| Eccentricity: | 0.0003643 |
| inclination: | 97.7613° |
| perigee height: | 590 km |
| apogee height: | 595 km |
| right ascension of ascending node: | 103.9926° |
| argument of perigee: | 88.2498° |
| revolutions per day: | 14.91639320 |
| mean anomaly at epoch: | 271.9137° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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