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 68506U 26145.59836547 +.00000000 +00000-0 +35783-3 0 00002
2 68506 97.4505 104.3788 0004209 134.3215 225.8365 15.18637271 04
| Epoch (UTC): | 25 May 2026 14:21:38 |
| Eccentricity: | 0.0004209 |
| inclination: | 97.4505° |
| perigee height: | 507 km |
| apogee height: | 513 km |
| right ascension of ascending node: | 104.3788° |
| argument of perigee: | 134.3215° |
| revolutions per day: | 15.18637271 |
| mean anomaly at epoch: | 225.8365° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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