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 68900U 26145.26658663 +.00000000 +00000-0 +50049-3 0 00007
2 68900 97.2871 340.9589 0001471 93.7476 266.3943 15.49213709 00
| Epoch (UTC): | 25 May 2026 06:23:53 |
| Eccentricity: | 0.0001471 |
| inclination: | 97.2871° |
| perigee height: | 418 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 340.9589° |
| argument of perigee: | 93.7476° |
| revolutions per day: | 15.49213709 |
| mean anomaly at epoch: | 266.3943° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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