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 69011U 26145.57930926 +.00000000 +00000-0 +20135-3 0 00003
2 69011 97.4072 43.8163 0006433 106.6781 253.5161 15.20396110 09
| Epoch (UTC): | 25 May 2026 13:54:12 |
| Eccentricity: | 0.0006433 |
| inclination: | 97.4072° |
| perigee height: | 500 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 43.8163° |
| argument of perigee: | 106.6781° |
| revolutions per day: | 15.20396110 |
| mean anomaly at epoch: | 253.5161° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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