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 45164U 26145.66168624 +.00000000 +00000-0 -18608-2 0 00006
2 45164 87.8859 40.7565 0002116 86.8277 273.3092 13.10373963 04
| Epoch (UTC): | 25 May 2026 15:52:49 |
| Eccentricity: | 0.0002116 |
| inclination: | 87.8859° |
| perigee height: | 1220 km |
| apogee height: | 1223 km |
| right ascension of ascending node: | 40.7565° |
| argument of perigee: | 86.8277° |
| revolutions per day: | 13.10373963 |
| mean anomaly at epoch: | 273.3092° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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