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 22803U 26039.53856064 +.00000000 +00000-0 +95937-4 0 00002
2 22803 70.9892 72.6030 0019494 256.5658 103.3293 14.17227498 00
| Epoch (UTC): | 08 February 2026 12:55:31 |
| Eccentricity: | 0.0019494 |
| inclination: | 70.9892° |
| perigee height: | 821 km |
| apogee height: | 849 km |
| right ascension of ascending node: | 72.6030° |
| argument of perigee: | 256.5658° |
| revolutions per day: | 14.17227498 |
| mean anomaly at epoch: | 103.3293° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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