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 33053U 26106.08261883 +.00000000 +00000-0 +77465-4 0 00001
2 33053 25.5824 275.5921 0007923 317.0677 42.9243 15.23609133 02
| Epoch (UTC): | 16 April 2026 01:58:58 |
| Eccentricity: | 0.0007923 |
| inclination: | 25.5824° |
| perigee height: | 490 km |
| apogee height: | 500 km |
| right ascension of ascending node: | 275.5921° |
| argument of perigee: | 317.0677° |
| revolutions per day: | 15.23609133 |
| mean anomaly at epoch: | 42.9243° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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