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 68748U 26145.37397605 +.00000000 +00000-0 +48749-3 0 00009
2 68748 97.2859 8.9174 0001372 100.2579 259.8827 15.49210211 08
| Epoch (UTC): | 25 May 2026 08:58:31 |
| Eccentricity: | 0.0001372 |
| inclination: | 97.2859° |
| perigee height: | 418 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 8.9174° |
| argument of perigee: | 100.2579° |
| revolutions per day: | 15.49210211 |
| mean anomaly at epoch: | 259.8827° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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