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 63875U 26145.12004608 +.00000000 +00000-0 +29955-3 0 00004
2 63875 70.0017 41.6744 0002523 268.6787 91.4083 14.98337355 01
| Epoch (UTC): | 25 May 2026 02:52:51 |
| Eccentricity: | 0.0002523 |
| inclination: | 70.0017° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 41.6744° |
| argument of perigee: | 268.6787° |
| revolutions per day: | 14.98337355 |
| mean anomaly at epoch: | 91.4083° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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