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 65541U 26145.46407027 +.00000000 +00000-0 +12921-2 0 00009
2 65541 97.4499 215.1078 0001884 109.8428 250.3003 15.05666842 08
| Epoch (UTC): | 25 May 2026 11:08:15 |
| Eccentricity: | 0.0001884 |
| inclination: | 97.4499° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 215.1078° |
| argument of perigee: | 109.8428° |
| revolutions per day: | 15.05666842 |
| mean anomaly at epoch: | 250.3003° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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