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 37214U 26150.57384663 +.00000000 +00000-0 +35489-3 0 00008
2 37214 98.9634 196.5127 0021177 235.2015 290.1489 14.14838967 09
| Epoch (UTC): | 30 May 2026 13:46:20 |
| Eccentricity: | 0.0021177 |
| inclination: | 98.9634° |
| perigee height: | 828 km |
| apogee height: | 858 km |
| right ascension of ascending node: | 196.5127° |
| argument of perigee: | 235.2015° |
| revolutions per day: | 14.14838967 |
| mean anomaly at epoch: | 290.1489° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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