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 65530U 26145.46128502 +.00000000 +00000-0 +31025-3 0 00002
2 65530 97.4490 215.1134 0000803 202.4650 157.6542 15.05656639 07
| Epoch (UTC): | 25 May 2026 11:04:15 |
| Eccentricity: | 0.0000803 |
| inclination: | 97.4490° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 215.1134° |
| argument of perigee: | 202.4650° |
| revolutions per day: | 15.05656639 |
| mean anomaly at epoch: | 157.6542° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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