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 65794U 26145.56199073 +.00000000 +00000-0 +21971-3 0 00005
2 65794 97.4532 8.2878 0003019 64.2097 295.9441 15.05667406 01
| Epoch (UTC): | 25 May 2026 13:29:15 |
| Eccentricity: | 0.0003019 |
| inclination: | 97.4532° |
| perigee height: | 547 km |
| apogee height: | 552 km |
| right ascension of ascending node: | 8.2878° |
| argument of perigee: | 64.2097° |
| revolutions per day: | 15.05667406 |
| mean anomaly at epoch: | 295.9441° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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