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 63163U 26145.45065383 +.00000000 +00000-0 +52919-4 0 00004
2 63163 88.9696 299.8134 0012630 292.0103 67.9731 13.96191947 05
| Epoch (UTC): | 25 May 2026 10:48:56 |
| Eccentricity: | 0.0012630 |
| inclination: | 88.9696° |
| perigee height: | 898 km |
| apogee height: | 916 km |
| right ascension of ascending node: | 299.8134° |
| argument of perigee: | 292.0103° |
| revolutions per day: | 13.96191947 |
| mean anomaly at epoch: | 67.9731° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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