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 68329U 26144.00046503 +.00000000 +00000-0 -27588-2 0 00009
2 68329 53.1611 354.3575 0000994 108.3490 251.7628 15.49429226 01
| Epoch (UTC): | 24 May 2026 00:00:40 |
| Eccentricity: | 0.0000994 |
| inclination: | 53.1611° |
| perigee height: | 418 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 354.3575° |
| argument of perigee: | 108.3490° |
| revolutions per day: | 15.49429226 |
| mean anomaly at epoch: | 251.7628° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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