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 69091U 26145.59111112 +.00000000 +00000-0 +42700-4 0 00004
2 69091 89.0139 344.1292 0094729 62.4148 298.6644 14.57450285 08
| Epoch (UTC): | 25 May 2026 14:11:12 |
| Eccentricity: | 0.0094729 |
| inclination: | 89.0139° |
| perigee height: | 634 km |
| apogee height: | 768 km |
| right ascension of ascending node: | 344.1292° |
| argument of perigee: | 62.4148° |
| revolutions per day: | 14.57450285 |
| mean anomaly at epoch: | 298.6644° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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