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 65654U 26145.40688588 +.00000000 +00000-0 +13022-2 0 00004
2 65654 97.4513 189.2803 0001890 119.6011 240.5405 15.05681285 06
| Epoch (UTC): | 25 May 2026 09:45:54 |
| Eccentricity: | 0.0001890 |
| inclination: | 97.4513° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 189.2803° |
| argument of perigee: | 119.6011° |
| revolutions per day: | 15.05681285 |
| mean anomaly at epoch: | 240.5405° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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