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 63237U 26145.15794436 +.00000000 +00000-0 +51499-3 0 00002
2 63237 97.3967 40.5389 0004981 204.9300 155.1701 15.31084761 09
| Epoch (UTC): | 25 May 2026 03:47:26 |
| Eccentricity: | 0.0004981 |
| inclination: | 97.3967° |
| perigee height: | 469 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 40.5389° |
| argument of perigee: | 204.9300° |
| revolutions per day: | 15.31084761 |
| mean anomaly at epoch: | 155.1701° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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