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 69015U 26145.43632559 +.00000000 +00000-0 +36241-3 0 00008
2 69015 97.4029 43.6785 0010106 116.6787 243.5485 15.21257975 06
| Epoch (UTC): | 25 May 2026 10:28:18 |
| Eccentricity: | 0.0010106 |
| inclination: | 97.4029° |
| perigee height: | 495 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 43.6785° |
| argument of perigee: | 116.6787° |
| revolutions per day: | 15.21257975 |
| mean anomaly at epoch: | 243.5485° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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