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 33312U 26150.45924034 +.00000000 +00000-0 +11757-3 0 00004
2 33312 97.4243 180.9471 0016224 281.9944 77.9464 15.05250679 02
| Epoch (UTC): | 30 May 2026 11:01:18 |
| Eccentricity: | 0.0016224 |
| inclination: | 97.4243° |
| perigee height: | 539 km |
| apogee height: | 562 km |
| right ascension of ascending node: | 180.9471° |
| argument of perigee: | 281.9944° |
| revolutions per day: | 15.05250679 |
| mean anomaly at epoch: | 77.9464° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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