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 26106.59691675 +.00000000 +00000-0 +55327-4 0 00006
2 03669 88.4466 151.1658 1707396 12.6822 351.2077 11.30422974 01
| Epoch (UTC): | 16 April 2026 14:19:33 |
| Eccentricity: | 0.1707396 |
| inclination: | 88.4466° |
| perigee height: | 576 km |
| apogee height: | 3440 km |
| right ascension of ascending node: | 151.1658° |
| argument of perigee: | 12.6822° |
| revolutions per day: | 11.30422974 |
| mean anomaly at epoch: | 351.2077° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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