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 65069U 26145.14761532 +.00000000 +00000-0 +45904-3 0 00001
2 65069 97.4497 222.2022 0002195 158.5745 201.5574 15.05660715 02
| Epoch (UTC): | 25 May 2026 03:32:33 |
| Eccentricity: | 0.0002195 |
| inclination: | 97.4497° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 222.2022° |
| argument of perigee: | 158.5745° |
| revolutions per day: | 15.05660715 |
| mean anomaly at epoch: | 201.5574° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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