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 00029U 26129.48305829 +.00000000 +00000-0 +64935-4 0 00004
2 00029 48.3775 208.5800 0021545 102.5869 257.7456 14.78728991 00
| Epoch (UTC): | 09 May 2026 11:35:36 |
| Eccentricity: | 0.0021545 |
| inclination: | 48.3775° |
| perigee height: | 618 km |
| apogee height: | 648 km |
| right ascension of ascending node: | 208.5800° |
| argument of perigee: | 102.5869° |
| revolutions per day: | 14.78728991 |
| mean anomaly at epoch: | 257.7456° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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