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 63271U 26145.61746448 +.00000000 +00000-0 +12867-2 0 00006
2 63271 42.9968 8.9474 0000225 149.4456 210.6425 15.70953063 02
| Epoch (UTC): | 25 May 2026 14:49:08 |
| Eccentricity: | 0.0000225 |
| inclination: | 42.9968° |
| perigee height: | 356 km |
| apogee height: | 356 km |
| right ascension of ascending node: | 8.9474° |
| argument of perigee: | 149.4456° |
| revolutions per day: | 15.70953063 |
| mean anomaly at epoch: | 210.6425° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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