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 65384U 26145.35767209 +.00000000 +00000-0 +23530-3 0 00002
2 65384 97.4474 16.6802 0002417 85.5912 274.5591 15.05656796 03
| Epoch (UTC): | 25 May 2026 08:35:02 |
| Eccentricity: | 0.0002417 |
| inclination: | 97.4474° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 16.6802° |
| argument of perigee: | 85.5912° |
| revolutions per day: | 15.05656796 |
| mean anomaly at epoch: | 274.5591° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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