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 63878U 26145.42481626 +.00000000 +00000-0 +45925-4 0 00005
2 63878 70.0026 41.1248 0002692 268.2185 91.8666 14.98334551 09
| Epoch (UTC): | 25 May 2026 10:11:44 |
| Eccentricity: | 0.0002692 |
| inclination: | 70.0026° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 41.1248° |
| argument of perigee: | 268.2185° |
| revolutions per day: | 14.98334551 |
| mean anomaly at epoch: | 91.8666° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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