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 63389U 26145.17558451 +.00000000 +00000-0 +49935-3 0 00009
2 63389 53.1587 56.9165 0001040 85.7959 274.3161 15.31718807 05
| Epoch (UTC): | 25 May 2026 04:12:50 |
| Eccentricity: | 0.0001040 |
| inclination: | 53.1587° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 56.9165° |
| argument of perigee: | 85.7959° |
| revolutions per day: | 15.31718807 |
| mean anomaly at epoch: | 274.3161° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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