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 22638U 26140.00009856 +.00000000 +00000-0 +37162-4 0 00008
2 22638 69.9218 0.9349 0060164 199.4843 160.3983 14.33659230 04
| Epoch (UTC): | 20 May 2026 00:00:08 |
| Eccentricity: | 0.0060164 |
| inclination: | 69.9218° |
| perigee height: | 736 km |
| apogee height: | 823 km |
| right ascension of ascending node: | 0.9349° |
| argument of perigee: | 199.4843° |
| revolutions per day: | 14.33659230 |
| mean anomaly at epoch: | 160.3983° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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