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 37224U 26069.93751944 +.00000000 +00000-0 +26625-3 0 00000
2 37224 71.9708 302.8181 0016842 254.5069 105.4241 14.93288098 06
| Epoch (UTC): | 10 March 2026 22:30:01 |
| Eccentricity: | 0.0016842 |
| inclination: | 71.9708° |
| perigee height: | 576 km |
| apogee height: | 599 km |
| right ascension of ascending node: | 302.8181° |
| argument of perigee: | 254.5069° |
| revolutions per day: | 14.93288098 |
| mean anomaly at epoch: | 105.4241° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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