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 58665U 26144.89988362 +.00000000 +00000-0 +17501-2 0 00009
2 58665 97.5278 238.1173 0010307 261.3121 98.6985 15.92638401 06
| Epoch (UTC): | 24 May 2026 21:35:49 |
| Eccentricity: | 0.0010307 |
| inclination: | 97.5278° |
| perigee height: | 288 km |
| apogee height: | 302 km |
| right ascension of ascending node: | 238.1173° |
| argument of perigee: | 261.3121° |
| revolutions per day: | 15.92638401 |
| mean anomaly at epoch: | 98.6985° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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