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 33495U 26102.15658721 +.00000000 +00000-0 +44596-4 0 00005
2 33495 98.1271 7.5738 0006483 235.9194 124.1399 14.74749167 07
| Epoch (UTC): | 12 April 2026 03:45:29 |
| Eccentricity: | 0.0006483 |
| inclination: | 98.1271° |
| perigee height: | 641 km |
| apogee height: | 651 km |
| right ascension of ascending node: | 7.5738° |
| argument of perigee: | 235.9194° |
| revolutions per day: | 14.74749167 |
| mean anomaly at epoch: | 124.1399° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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