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 65294U 26145.41856823 +.00000000 +00000-0 +53567-3 0 00003
2 65294 97.4485 197.8787 0001382 181.9281 178.1942 15.05665242 04
| Epoch (UTC): | 25 May 2026 10:02:44 |
| Eccentricity: | 0.0001382 |
| inclination: | 97.4485° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 197.8787° |
| argument of perigee: | 181.9281° |
| revolutions per day: | 15.05665242 |
| mean anomaly at epoch: | 178.1942° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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