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 37152U 26032.37310985 +.00000000 +00000-0 +61858-4 0 00002
2 37152 82.4599 149.9841 0001837 104.7309 310.5518 12.42982004 01
| Epoch (UTC): | 01 February 2026 08:57:16 |
| Eccentricity: | 0.0001837 |
| inclination: | 82.4599° |
| perigee height: | 1493 km |
| apogee height: | 1495 km |
| right ascension of ascending node: | 149.9841° |
| argument of perigee: | 104.7309° |
| revolutions per day: | 12.42982004 |
| mean anomaly at epoch: | 310.5518° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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