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 37227U 26109.82936825 +.00000000 +00000-0 +89419-4 0 00000
2 37227 71.9653 266.3488 0016288 228.4668 131.5101 14.85152054 09
| Epoch (UTC): | 19 April 2026 19:54:17 |
| Eccentricity: | 0.0016288 |
| inclination: | 71.9653° |
| perigee height: | 602 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 266.3488° |
| argument of perigee: | 228.4668° |
| revolutions per day: | 14.85152054 |
| mean anomaly at epoch: | 131.5101° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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