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 26047.12180556 +.00000000 +00000-0 +61851-3 0 00008
2 00022 50.2478 337.6270 0083092 357.4388 2.6135 15.25930264 04
| Epoch (UTC): | 16 February 2026 02:55:24 |
| Eccentricity: | 0.0083092 |
| inclination: | 50.2478° |
| perigee height: | 431 km |
| apogee height: | 545 km |
| right ascension of ascending node: | 337.6270° |
| argument of perigee: | 357.4388° |
| revolutions per day: | 15.25930264 |
| mean anomaly at epoch: | 2.6135° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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