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 51878U 26145.10697574 +.00000000 +00000-0 -85276-4 0 00002
2 51878 53.2132 26.0680 0001833 89.5352 270.5850 15.08851412 08
| Epoch (UTC): | 25 May 2026 02:34:02 |
| Eccentricity: | 0.0001833 |
| inclination: | 53.2132° |
| perigee height: | 538 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 26.0680° |
| argument of perigee: | 89.5352° |
| revolutions per day: | 15.08851412 |
| mean anomaly at epoch: | 270.5850° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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