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 62649U 26145.19423907 +.00000000 +00000-0 +73208-3 0 00006
2 62649 97.4027 232.3329 0001729 75.0989 285.0451 15.44036375 02
| Epoch (UTC): | 25 May 2026 04:39:42 |
| Eccentricity: | 0.0001729 |
| inclination: | 97.4027° |
| perigee height: | 433 km |
| apogee height: | 435 km |
| right ascension of ascending node: | 232.3329° |
| argument of perigee: | 75.0989° |
| revolutions per day: | 15.44036375 |
| mean anomaly at epoch: | 285.0451° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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