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 69008U 26145.47719624 +.00000000 +00000-0 +14306-3 0 00001
2 69008 97.7371 43.3339 0003032 206.5174 153.5890 14.91029140 09
| Epoch (UTC): | 25 May 2026 11:27:09 |
| Eccentricity: | 0.0003032 |
| inclination: | 97.7371° |
| perigee height: | 593 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 43.3339° |
| argument of perigee: | 206.5174° |
| revolutions per day: | 14.91029140 |
| mean anomaly at epoch: | 153.5890° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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