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 65385U 26145.60689486 +.00000000 +00000-0 +10168-3 0 00004
2 65385 97.4487 16.9601 0002471 85.7962 274.3548 15.05654150 07
| Epoch (UTC): | 25 May 2026 14:33:55 |
| Eccentricity: | 0.0002471 |
| inclination: | 97.4487° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 16.9601° |
| argument of perigee: | 85.7962° |
| revolutions per day: | 15.05654150 |
| mean anomaly at epoch: | 274.3548° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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