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 00340U 26087.36636366 +.00000000 +00000-0 +46851-3 0 00009
2 00340 44.7961 110.4478 2425817 341.5087 20.2402 9.12889336 01
| Epoch (UTC): | 28 March 2026 08:47:33 |
| Eccentricity: | 0.2425817 |
| inclination: | 44.7961° |
| perigee height: | 947 km |
| apogee height: | 5638 km |
| right ascension of ascending node: | 110.4478° |
| argument of perigee: | 341.5087° |
| revolutions per day: | 9.12889336 |
| mean anomaly at epoch: | 20.2402° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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