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 21152U 26053.68964699 +.00000000 +00000-0 +46008-4 0 00009
2 21152 82.9270 28.7121 0042566 37.5604 152.0814 13.74491919 09
| Epoch (UTC): | 22 February 2026 16:33:05 |
| Eccentricity: | 0.0042566 |
| inclination: | 82.9270° |
| perigee height: | 952 km |
| apogee height: | 1015 km |
| right ascension of ascending node: | 28.7121° |
| argument of perigee: | 37.5604° |
| revolutions per day: | 13.74491919 |
| mean anomaly at epoch: | 152.0814° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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