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 65388U 26145.58197609 +.00000000 +00000-0 +50983-4 0 00005
2 65388 97.4532 16.9968 0002188 87.7802 272.3676 15.05656457 09
| Epoch (UTC): | 25 May 2026 13:58:02 |
| Eccentricity: | 0.0002188 |
| inclination: | 97.4532° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 16.9968° |
| argument of perigee: | 87.7802° |
| revolutions per day: | 15.05656457 |
| mean anomaly at epoch: | 272.3676° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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