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 33374U 26044.73575451 +.00000000 +00000-0 +16456-2 0 00000
2 33374 49.4353 204.7194 5367931 199.4164 128.0496 4.95947027 02
| Epoch (UTC): | 13 February 2026 17:39:29 |
| Eccentricity: | 0.5367931 |
| inclination: | 49.4353° |
| perigee height: | 350 km |
| apogee height: | 15944 km |
| right ascension of ascending node: | 204.7194° |
| argument of perigee: | 199.4164° |
| revolutions per day: | 4.95947027 |
| mean anomaly at epoch: | 128.0496° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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