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 26065.23016656 +.00000000 +00000-0 -30329-4 0 00008
2 22803 70.9924 18.4206 0018709 221.4934 138.4770 14.17232164 00
| Epoch (UTC): | 06 March 2026 05:31:26 |
| Eccentricity: | 0.0018709 |
| inclination: | 70.9924° |
| perigee height: | 821 km |
| apogee height: | 848 km |
| right ascension of ascending node: | 18.4206° |
| argument of perigee: | 221.4934° |
| revolutions per day: | 14.17232164 |
| mean anomaly at epoch: | 138.4770° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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