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 69020U 26145.65812941 +.00000000 +00000-0 +39117-3 0 00008
2 69020 97.4068 43.8598 0005978 69.4748 290.7128 15.19577851 05
| Epoch (UTC): | 25 May 2026 15:47:42 |
| Eccentricity: | 0.0005978 |
| inclination: | 97.4068° |
| perigee height: | 503 km |
| apogee height: | 511 km |
| right ascension of ascending node: | 43.8598° |
| argument of perigee: | 69.4748° |
| revolutions per day: | 15.19577851 |
| mean anomaly at epoch: | 290.7128° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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