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 65449U 26145.52264068 +.00000000 +00000-0 +23791-3 0 00007
2 65449 97.4495 359.8130 0002759 91.1096 269.0448 15.05656581 01
| Epoch (UTC): | 25 May 2026 12:32:36 |
| Eccentricity: | 0.0002759 |
| inclination: | 97.4495° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 359.8130° |
| argument of perigee: | 91.1096° |
| revolutions per day: | 15.05656581 |
| mean anomaly at epoch: | 269.0448° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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