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 65455U 26145.57801103 +.00000000 +00000-0 +22226-3 0 00008
2 65455 97.4492 359.7374 0002491 80.3417 279.8091 15.05658680 09
| Epoch (UTC): | 25 May 2026 13:52:20 |
| Eccentricity: | 0.0002491 |
| inclination: | 97.4492° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 359.7374° |
| argument of perigee: | 80.3417° |
| revolutions per day: | 15.05658680 |
| mean anomaly at epoch: | 279.8091° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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