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 63870U 26145.12855782 +.00000000 +00000-0 +28958-3 0 00008
2 63870 70.0022 41.6987 0002695 269.8477 90.2373 14.98338223 04
| Epoch (UTC): | 25 May 2026 03:05:07 |
| Eccentricity: | 0.0002695 |
| inclination: | 70.0022° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 41.6987° |
| argument of perigee: | 269.8477° |
| revolutions per day: | 14.98338223 |
| mean anomaly at epoch: | 90.2373° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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