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 36745U 26145.58979513 +.00000000 +00000-0 +00000-0 0 00003
2 36745 0.0743 53.8637 0005189 34.4124 37.7352 1.00269365 03
| Epoch (UTC): | 25 May 2026 14:09:18 |
| Eccentricity: | 0.0005189 |
| inclination: | 0.0743° |
| perigee height: | 35765 km |
| apogee height: | 35809 km |
| right ascension of ascending node: | 53.8637° |
| argument of perigee: | 34.4124° |
| revolutions per day: | 1.00269365 |
| mean anomaly at epoch: | 37.7352° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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