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 65394U 26145.61796897 +.00000000 +00000-0 +19967-3 0 00006
2 65394 97.4480 16.9434 0002698 70.3760 289.7758 15.05657146 02
| Epoch (UTC): | 25 May 2026 14:49:52 |
| Eccentricity: | 0.0002698 |
| inclination: | 97.4480° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 16.9434° |
| argument of perigee: | 70.3760° |
| revolutions per day: | 15.05657146 |
| mean anomaly at epoch: | 289.7758° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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