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 21087U 26112.10136977 +.00000000 +00000-0 +26624-4 0 00001
2 21087 82.9450 166.7387 0035863 34.7526 352.1770 13.75519135 03
| Epoch (UTC): | 22 April 2026 02:25:58 |
| Eccentricity: | 0.0035863 |
| inclination: | 82.9450° |
| perigee height: | 953 km |
| apogee height: | 1006 km |
| right ascension of ascending node: | 166.7387° |
| argument of perigee: | 34.7526° |
| revolutions per day: | 13.75519135 |
| mean anomaly at epoch: | 352.1770° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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