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 22829U 26155.08258238 +.00000000 +00000-0 +71369-4 0 00001
2 22829 98.6661 222.1782 0010782 71.0926 289.1425 14.31914746 09
| Epoch (UTC): | 04 June 2026 01:58:55 |
| Eccentricity: | 0.0010782 |
| inclination: | 98.6661° |
| perigee height: | 778 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 222.1782° |
| argument of perigee: | 71.0926° |
| revolutions per day: | 14.31914746 |
| mean anomaly at epoch: | 289.1425° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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