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 22161U 26160.02321153 +.00000000 +00000-0 +11908-3 0 00009
2 22161 62.9992 263.2962 0728846 239.7624 112.9315 13.32850667 02
| Epoch (UTC): | 09 June 2026 00:33:25 |
| Eccentricity: | 0.0728846 |
| inclination: | 62.9992° |
| perigee height: | 588 km |
| apogee height: | 1684 km |
| right ascension of ascending node: | 263.2962° |
| argument of perigee: | 239.7624° |
| revolutions per day: | 13.32850667 |
| mean anomaly at epoch: | 112.9315° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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