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 37153U 26053.89158256 +.00000000 +00000-0 +26744-3 0 00008
2 37153 82.4613 149.6203 0006814 338.5595 21.5197 12.40789699 07
| Epoch (UTC): | 22 February 2026 21:23:52 |
| Eccentricity: | 0.0006814 |
| inclination: | 82.4613° |
| perigee height: | 1498 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 149.6203° |
| argument of perigee: | 338.5595° |
| revolutions per day: | 12.40789699 |
| mean anomaly at epoch: | 21.5197° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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