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 22237U 26106.94161946 +.00000000 +00000-0 +25306-4 0 00004
2 22237 82.5138 354.5579 0020553 89.0355 271.3213 14.80344023 06
| Epoch (UTC): | 16 April 2026 22:35:55 |
| Eccentricity: | 0.0020553 |
| inclination: | 82.5138° |
| perigee height: | 614 km |
| apogee height: | 643 km |
| right ascension of ascending node: | 354.5579° |
| argument of perigee: | 89.0355° |
| revolutions per day: | 14.80344023 |
| mean anomaly at epoch: | 271.3213° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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