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 68455U 26145.37319758 +.00000000 +00000-0 +23070-3 0 00007
2 68455 97.4562 104.1090 0007076 130.6162 229.5688 15.17146754 08
| Epoch (UTC): | 25 May 2026 08:57:24 |
| Eccentricity: | 0.0007076 |
| inclination: | 97.4562° |
| perigee height: | 510 km |
| apogee height: | 519 km |
| right ascension of ascending node: | 104.1090° |
| argument of perigee: | 130.6162° |
| revolutions per day: | 15.17146754 |
| mean anomaly at epoch: | 229.5688° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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