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 63677U 26145.48873769 +.00000000 +00000-0 +61228-3 0 00004
2 63677 42.9967 317.3451 0000481 268.9033 91.1764 15.27593795 07
| Epoch (UTC): | 25 May 2026 11:43:46 |
| Eccentricity: | 0.0000481 |
| inclination: | 42.9967° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 317.3451° |
| argument of perigee: | 268.9033° |
| revolutions per day: | 15.27593795 |
| mean anomaly at epoch: | 91.1764° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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