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 26108.96389975 +.00000000 +00000-0 +10752-2 0 00002
2 37153 82.4523 115.3166 0006924 203.7685 156.3074 12.40791605 01
| Epoch (UTC): | 18 April 2026 23:08:00 |
| Eccentricity: | 0.0006924 |
| inclination: | 82.4523° |
| perigee height: | 1498 km |
| apogee height: | 1509 km |
| right ascension of ascending node: | 115.3166° |
| argument of perigee: | 203.7685° |
| revolutions per day: | 12.40791605 |
| mean anomaly at epoch: | 156.3074° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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