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 33492U 26145.57006404 +.00000000 +00000-0 +39001-4 0 00005
2 33492 98.0867 256.9373 0001534 98.7605 261.3773 14.67538852 02
| Epoch (UTC): | 25 May 2026 13:40:53 |
| Eccentricity: | 0.0001534 |
| inclination: | 98.0867° |
| perigee height: | 668 km |
| apogee height: | 670 km |
| right ascension of ascending node: | 256.9373° |
| argument of perigee: | 98.7605° |
| revolutions per day: | 14.67538852 |
| mean anomaly at epoch: | 261.3773° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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