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 26101.88121721 +.00000000 +00000-0 +93624-4 0 00002
2 37227 71.9652 284.1172 0016591 241.8740 118.0750 14.85141559 01
| Epoch (UTC): | 11 April 2026 21:08:57 |
| Eccentricity: | 0.0016591 |
| inclination: | 71.9652° |
| perigee height: | 602 km |
| apogee height: | 625 km |
| right ascension of ascending node: | 284.1172° |
| argument of perigee: | 241.8740° |
| revolutions per day: | 14.85141559 |
| mean anomaly at epoch: | 118.0750° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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