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 63364U 26145.45862666 +.00000000 +00000-0 +68915-3 0 00008
2 63364 53.1610 53.0129 0001390 97.5630 262.5528 15.30209077 07
| Epoch (UTC): | 25 May 2026 11:00:25 |
| Eccentricity: | 0.0001390 |
| inclination: | 53.1610° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 53.0129° |
| argument of perigee: | 97.5630° |
| revolutions per day: | 15.30209077 |
| mean anomaly at epoch: | 262.5528° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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