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 37225U 26145.28271071 +.00000000 +00000-0 +51706-4 0 00001
2 37225 71.9718 210.6571 0016410 178.2293 181.8932 14.82112691 07
| Epoch (UTC): | 25 May 2026 06:47:06 |
| Eccentricity: | 0.0016410 |
| inclination: | 71.9718° |
| perigee height: | 611 km |
| apogee height: | 634 km |
| right ascension of ascending node: | 210.6571° |
| argument of perigee: | 178.2293° |
| revolutions per day: | 14.82112691 |
| mean anomaly at epoch: | 181.8932° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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