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 65877U 26145.13645863 +.00000000 +00000-0 +51794-3 0 00009
2 65877 53.1614 298.8216 0001254 90.1351 269.9793 15.30205533 04
| Epoch (UTC): | 25 May 2026 03:16:30 |
| Eccentricity: | 0.0001254 |
| inclination: | 53.1614° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 298.8216° |
| argument of perigee: | 90.1351° |
| revolutions per day: | 15.30205533 |
| mean anomaly at epoch: | 269.9793° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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