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 63879U 26145.13256704 +.00000000 +00000-0 +28051-3 0 00001
2 63879 70.0022 41.7119 0002565 269.4363 90.6502 14.98337849 08
| Epoch (UTC): | 25 May 2026 03:10:53 |
| Eccentricity: | 0.0002565 |
| inclination: | 70.0022° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 41.7119° |
| argument of perigee: | 269.4363° |
| revolutions per day: | 14.98337849 |
| mean anomaly at epoch: | 90.6502° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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