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 18821U 26017.88375767 +.00000000 +00000-0 +31781-4 0 00004
2 18821 82.5417 85.2294 0015001 152.0232 208.1738 13.85218749 08
| Epoch (UTC): | 17 January 2026 21:12:36 |
| Eccentricity: | 0.0015001 |
| inclination: | 82.5417° |
| perigee height: | 934 km |
| apogee height: | 956 km |
| right ascension of ascending node: | 85.2294° |
| argument of perigee: | 152.0232° |
| revolutions per day: | 13.85218749 |
| mean anomaly at epoch: | 208.1738° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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