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 26073.28700530 +.00000000 +00000-0 +25501-3 0 00000
2 37224 71.9707 295.2361 0016732 248.9660 110.9721 14.93306403 07
| Epoch (UTC): | 14 March 2026 06:53:17 |
| Eccentricity: | 0.0016732 |
| inclination: | 71.9707° |
| perigee height: | 576 km |
| apogee height: | 599 km |
| right ascension of ascending node: | 295.2361° |
| argument of perigee: | 248.9660° |
| revolutions per day: | 14.93306403 |
| mean anomaly at epoch: | 110.9721° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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