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 63273U 26145.62264361 +.00000000 +00000-0 +21233-2 0 00005
2 63273 43.0000 8.0906 0002206 245.1083 114.9555 15.70969627 08
| Epoch (UTC): | 25 May 2026 14:56:36 |
| Eccentricity: | 0.0002206 |
| inclination: | 43.0000° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 8.0906° |
| argument of perigee: | 245.1083° |
| revolutions per day: | 15.70969627 |
| mean anomaly at epoch: | 114.9555° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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