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 67800U 26145.46381259 +.00000000 +00000-0 +71343-3 0 00001
2 67800 97.2862 333.5118 0002451 76.1388 284.0127 15.33463551 06
| Epoch (UTC): | 25 May 2026 11:07:53 |
| Eccentricity: | 0.0002451 |
| inclination: | 97.2862° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 333.5118° |
| argument of perigee: | 76.1388° |
| revolutions per day: | 15.33463551 |
| mean anomaly at epoch: | 284.0127° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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