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 68776U 26145.54198749 +.00000000 +00000-0 -10123-1 0 00001
2 68776 97.2851 182.4357 0000900 29.4280 330.7034 15.72508576 08
| Epoch (UTC): | 25 May 2026 13:00:27 |
| Eccentricity: | 0.0000900 |
| inclination: | 97.2851° |
| perigee height: | 351 km |
| apogee height: | 352 km |
| right ascension of ascending node: | 182.4357° |
| argument of perigee: | 29.4280° |
| revolutions per day: | 15.72508576 |
| mean anomaly at epoch: | 330.7034° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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