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 63773U 26145.53809847 +.00000000 +00000-0 +74902-3 0 00006
2 63773 42.9997 330.9658 0001141 274.4562 85.6160 15.27590247 07
| Epoch (UTC): | 25 May 2026 12:54:51 |
| Eccentricity: | 0.0001141 |
| inclination: | 42.9997° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 330.9658° |
| argument of perigee: | 274.4562° |
| revolutions per day: | 15.27590247 |
| mean anomaly at epoch: | 85.6160° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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