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 00876U 26158.91339419 +.00000000 +00000-0 +36605-4 0 00009
2 00876 65.0606 353.1148 0151952 266.4572 91.9142 14.65731352 09
| Epoch (UTC): | 07 June 2026 21:55:17 |
| Eccentricity: | 0.0151952 |
| inclination: | 65.0606° |
| perigee height: | 568 km |
| apogee height: | 782 km |
| right ascension of ascending node: | 353.1148° |
| argument of perigee: | 266.4572° |
| revolutions per day: | 14.65731352 |
| mean anomaly at epoch: | 91.9142° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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