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 26067.00546992 +.00000000 +00000-0 +65914-4 0 00009
2 00876 65.0576 264.7113 0149944 298.6270 59.9819 14.65673648 02
| Epoch (UTC): | 08 March 2026 00:07:52 |
| Eccentricity: | 0.0149944 |
| inclination: | 65.0576° |
| perigee height: | 569 km |
| apogee height: | 781 km |
| right ascension of ascending node: | 264.7113° |
| argument of perigee: | 298.6270° |
| revolutions per day: | 14.65673648 |
| mean anomaly at epoch: | 59.9819° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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