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 03615U 26133.33955582 +.00000000 +00000-0 -39546-4 0 00005
2 03615 101.6990 83.0186 0032242 30.7878 329.5079 12.56249290 00
| Epoch (UTC): | 13 May 2026 08:08:57 |
| Eccentricity: | 0.0032242 |
| inclination: | 101.6990° |
| perigee height: | 1413 km |
| apogee height: | 1464 km |
| right ascension of ascending node: | 83.0186° |
| argument of perigee: | 30.7878° |
| revolutions per day: | 12.56249290 |
| mean anomaly at epoch: | 329.5079° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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