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 52878U 26145.38803522 +.00000000 +00000-0 +51086-4 0 00006
2 52878 53.2120 29.8070 0001166 86.9548 273.1577 15.08832205 01
| Epoch (UTC): | 25 May 2026 09:18:46 |
| Eccentricity: | 0.0001166 |
| inclination: | 53.2120° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 29.8070° |
| argument of perigee: | 86.9548° |
| revolutions per day: | 15.08832205 |
| mean anomaly at epoch: | 273.1577° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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