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 36037U 26032.47330071 +.00000000 +00000-0 +90513-4 0 00002
2 36037 98.2399 217.7177 0012787 344.9387 15.1428 14.54761810 04
| Epoch (UTC): | 01 February 2026 11:21:33 |
| Eccentricity: | 0.0012787 |
| inclination: | 98.2399° |
| perigee height: | 701 km |
| apogee height: | 719 km |
| right ascension of ascending node: | 217.7177° |
| argument of perigee: | 344.9387° |
| revolutions per day: | 14.54761810 |
| mean anomaly at epoch: | 15.1428° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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