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 22109U 26087.67086713 +.00000000 +00000-0 +19138-3 0 00003
2 22109 19.7814 93.4445 0031547 342.4996 17.4331 14.80092762 00
| Epoch (UTC): | 28 March 2026 16:06:02 |
| Eccentricity: | 0.0031547 |
| inclination: | 19.7814° |
| perigee height: | 607 km |
| apogee height: | 651 km |
| right ascension of ascending node: | 93.4445° |
| argument of perigee: | 342.4996° |
| revolutions per day: | 14.80092762 |
| mean anomaly at epoch: | 17.4331° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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