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 65798U 26145.54537832 +.00000000 +00000-0 +33949-3 0 00004
2 65798 97.4494 8.3115 0002508 94.9909 265.1605 15.05660293 09
| Epoch (UTC): | 25 May 2026 13:05:20 |
| Eccentricity: | 0.0002508 |
| inclination: | 97.4494° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 8.3115° |
| argument of perigee: | 94.9909° |
| revolutions per day: | 15.05660293 |
| mean anomaly at epoch: | 265.1605° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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