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 68033U 26145.61482943 +.00000000 +00000-0 +59506-3 0 00006
2 68033 97.2847 94.6513 0001634 85.7223 274.4207 15.33466615 04
| Epoch (UTC): | 25 May 2026 14:45:21 |
| Eccentricity: | 0.0001634 |
| inclination: | 97.2847° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 94.6513° |
| argument of perigee: | 85.7223° |
| revolutions per day: | 15.33466615 |
| mean anomaly at epoch: | 274.4207° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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