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 03669U 26088.19001347 +.00000000 +00000-0 +10247-3 0 00003
2 03669 88.4506 153.1804 1707830 49.8257 324.0243 11.30419292 00
| Epoch (UTC): | 29 March 2026 04:33:37 |
| Eccentricity: | 0.1707830 |
| inclination: | 88.4506° |
| perigee height: | 576 km |
| apogee height: | 3441 km |
| right ascension of ascending node: | 153.1804° |
| argument of perigee: | 49.8257° |
| revolutions per day: | 11.30419292 |
| mean anomaly at epoch: | 324.0243° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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