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 63238U 26145.45605118 +.00000000 +00000-0 +53306-3 0 00003
2 63238 97.3970 40.7615 0005120 204.8677 155.2318 15.30818712 05
| Epoch (UTC): | 25 May 2026 10:56:42 |
| Eccentricity: | 0.0005120 |
| inclination: | 97.3970° |
| perigee height: | 470 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 40.7615° |
| argument of perigee: | 204.8677° |
| revolutions per day: | 15.30818712 |
| mean anomaly at epoch: | 155.2318° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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