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 26162.15984898 +.00000000 +00000-0 +48351-4 0 00007
2 13033 82.9410 169.6896 0031566 204.0016 226.9266 13.73473394 02
| Epoch (UTC): | 11 June 2026 03:50:10 |
| Eccentricity: | 0.0031566 |
| inclination: | 82.9410° |
| perigee height: | 964 km |
| apogee height: | 1010 km |
| right ascension of ascending node: | 169.6896° |
| argument of perigee: | 204.0016° |
| revolutions per day: | 13.73473394 |
| mean anomaly at epoch: | 226.9266° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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