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 00733U 26040.68245855 +.00000000 +00000-0 +12153-3 0 00006
2 00733 99.1230 52.4946 0032582 341.7515 18.2496 14.34002663 04
| Epoch (UTC): | 09 February 2026 16:22:44 |
| Eccentricity: | 0.0032582 |
| inclination: | 99.1230° |
| perigee height: | 755 km |
| apogee height: | 802 km |
| right ascension of ascending node: | 52.4946° |
| argument of perigee: | 341.7515° |
| revolutions per day: | 14.34002663 |
| mean anomaly at epoch: | 18.2496° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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