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 13033U 26106.73802698 +.00000000 +00000-0 +27732-4 0 00006
2 13033 82.9445 210.6256 0032089 3.1492 148.9959 13.73468690 09
| Epoch (UTC): | 16 April 2026 17:42:45 |
| Eccentricity: | 0.0032089 |
| inclination: | 82.9445° |
| perigee height: | 964 km |
| apogee height: | 1011 km |
| right ascension of ascending node: | 210.6256° |
| argument of perigee: | 3.1492° |
| revolutions per day: | 13.73468690 |
| mean anomaly at epoch: | 148.9959° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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