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 45145U 26145.12724863 +.00000000 +00000-0 +11086-2 0 00001
2 45145 87.8923 25.6620 0002188 32.6163 327.5100 13.11414097 08
| Epoch (UTC): | 25 May 2026 03:03:14 |
| Eccentricity: | 0.0002188 |
| inclination: | 87.8923° |
| perigee height: | 1216 km |
| apogee height: | 1219 km |
| right ascension of ascending node: | 25.6620° |
| argument of perigee: | 32.6163° |
| revolutions per day: | 13.11414097 |
| mean anomaly at epoch: | 327.5100° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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