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 00022U 26073.83275725 +.00000000 +00000-0 +68747-3 0 00009
2 00022 50.2424 206.0331 0080428 104.7764 256.2124 15.26837350 01
| Epoch (UTC): | 14 March 2026 19:59:10 |
| Eccentricity: | 0.0080428 |
| inclination: | 50.2424° |
| perigee height: | 430 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 206.0331° |
| argument of perigee: | 104.7764° |
| revolutions per day: | 15.26837350 |
| mean anomaly at epoch: | 256.2124° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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