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 33496U 26038.71539257 +.00000000 +00000-0 +13091-3 0 00003
2 33496 98.1503 302.6732 0007171 72.8774 287.3219 14.74871260 09
| Epoch (UTC): | 07 February 2026 17:10:09 |
| Eccentricity: | 0.0007171 |
| inclination: | 98.1503° |
| perigee height: | 641 km |
| apogee height: | 651 km |
| right ascension of ascending node: | 302.6732° |
| argument of perigee: | 72.8774° |
| revolutions per day: | 14.74871260 |
| mean anomaly at epoch: | 287.3219° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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