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 26106.06595654 +.00000000 +00000-0 +48612-4 0 00007
2 03669 88.4466 151.2240 1707419 13.7544 350.4536 11.30422881 06
| Epoch (UTC): | 16 April 2026 01:34:58 |
| Eccentricity: | 0.1707419 |
| inclination: | 88.4466° |
| perigee height: | 576 km |
| apogee height: | 3440 km |
| right ascension of ascending node: | 151.2240° |
| argument of perigee: | 13.7544° |
| revolutions per day: | 11.30422881 |
| mean anomaly at epoch: | 350.4536° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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