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 62363U 26145.05512480 +.00000000 +00000-0 +00000-0 0 00006
2 62363 0.0225 319.5369 0006122 94.0248 306.4941 5.00115259 00
| Epoch (UTC): | 25 May 2026 01:19:22 |
| Eccentricity: | 0.0006122 |
| inclination: | 0.0225° |
| perigee height: | 8057 km |
| apogee height: | 8075 km |
| right ascension of ascending node: | 319.5369° |
| argument of perigee: | 94.0248° |
| revolutions per day: | 5.00115259 |
| mean anomaly at epoch: | 306.4941° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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