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 26150.51198557 +.00000000 +00000-0 +11816-3 0 00009
2 37227 71.9649 175.4077 0013707 154.4627 205.7219 14.85219981 01
| Epoch (UTC): | 30 May 2026 12:17:15 |
| Eccentricity: | 0.0013707 |
| inclination: | 71.9649° |
| perigee height: | 603 km |
| apogee height: | 622 km |
| right ascension of ascending node: | 175.4077° |
| argument of perigee: | 154.4627° |
| revolutions per day: | 14.85219981 |
| mean anomaly at epoch: | 205.7219° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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