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 24737U 26146.16225249 +.00000000 +00000-0 +00000-0 0 00006
2 24737 14.4280 3.9730 0011413 323.4334 216.4431 0.99027795 07
| Epoch (UTC): | 26 May 2026 03:53:38 |
| Eccentricity: | 0.0011413 |
| inclination: | 14.4280° |
| perigee height: | 36090 km |
| apogee height: | 36188 km |
| right ascension of ascending node: | 3.9730° |
| argument of perigee: | 323.4334° |
| revolutions per day: | 0.99027795 |
| mean anomaly at epoch: | 216.4431° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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