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 63089U 26145.48044198 +.00000000 +00000-0 +30437-3 0 00005
2 63089 70.0003 160.8705 0003903 263.6409 96.4306 14.98349103 00
| Epoch (UTC): | 25 May 2026 11:31:50 |
| Eccentricity: | 0.0003903 |
| inclination: | 70.0003° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 160.8705° |
| argument of perigee: | 263.6409° |
| revolutions per day: | 14.98349103 |
| mean anomaly at epoch: | 96.4306° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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