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 69101U 26135.82908955 +.00000000 +00000-0 +33338-4 0 00007
2 69101 97.5067 218.5063 0013930 282.6221 77.3451 15.11230034 04
| Epoch (UTC): | 15 May 2026 19:53:53 |
| Eccentricity: | 0.0013930 |
| inclination: | 97.5067° |
| perigee height: | 523 km |
| apogee height: | 542 km |
| right ascension of ascending node: | 218.5063° |
| argument of perigee: | 282.6221° |
| revolutions per day: | 15.11230034 |
| mean anomaly at epoch: | 77.3451° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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