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 22077U 26053.57038602 +.00000000 +00000-0 +11991-3 0 00002
2 22077 66.0853 161.2300 0012221 310.3664 65.5752 12.86609097 00
| Epoch (UTC): | 22 February 2026 13:41:21 |
| Eccentricity: | 0.0012221 |
| inclination: | 66.0853° |
| perigee height: | 1306 km |
| apogee height: | 1324 km |
| right ascension of ascending node: | 161.2300° |
| argument of perigee: | 310.3664° |
| revolutions per day: | 12.86609097 |
| mean anomaly at epoch: | 65.5752° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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