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 22343U 26088.11386970 +.00000000 +00000-0 +44606-3 0 00009
2 22343 70.9589 284.2259 0094966 303.3020 197.1933 14.12026235 00
| Epoch (UTC): | 29 March 2026 02:43:58 |
| Eccentricity: | 0.0094966 |
| inclination: | 70.9589° |
| perigee height: | 784 km |
| apogee height: | 921 km |
| right ascension of ascending node: | 284.2259° |
| argument of perigee: | 303.3020° |
| revolutions per day: | 14.12026235 |
| mean anomaly at epoch: | 197.1933° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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