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 33434U 26145.55964441 +.00000000 +00000-0 +80266-4 0 00002
2 33434 98.6151 172.0516 0013654 202.4816 157.5770 14.30148089 03
| Epoch (UTC): | 25 May 2026 13:25:53 |
| Eccentricity: | 0.0013654 |
| inclination: | 98.6151° |
| perigee height: | 781 km |
| apogee height: | 801 km |
| right ascension of ascending node: | 172.0516° |
| argument of perigee: | 202.4816° |
| revolutions per day: | 14.30148089 |
| mean anomaly at epoch: | 157.5770° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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