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 65527U 26145.15391657 +.00000000 +00000-0 +45492-4 0 00001
2 65527 97.4500 214.7569 0001624 147.9420 212.1906 15.05649186 02
| Epoch (UTC): | 25 May 2026 03:41:38 |
| Eccentricity: | 0.0001624 |
| inclination: | 97.4500° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 214.7569° |
| argument of perigee: | 147.9420° |
| revolutions per day: | 15.05649186 |
| mean anomaly at epoch: | 212.1906° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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