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 68309U 26145.30713116 +.00000000 +00000-0 +10470-2 0 00003
2 68309 97.2844 271.5183 0000805 84.1724 275.9633 15.75209792 00
| Epoch (UTC): | 25 May 2026 07:22:16 |
| Eccentricity: | 0.0000805 |
| inclination: | 97.2844° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 271.5183° |
| argument of perigee: | 84.1724° |
| revolutions per day: | 15.75209792 |
| mean anomaly at epoch: | 275.9633° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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