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 49766U 26145.29468428 +.00000000 +00000-0 +27296-4 0 00006
2 49766 53.2151 155.2343 0000896 81.3277 278.7817 15.08839956 09
| Epoch (UTC): | 25 May 2026 07:04:20 |
| Eccentricity: | 0.0000896 |
| inclination: | 53.2151° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 155.2343° |
| argument of perigee: | 81.3277° |
| revolutions per day: | 15.08839956 |
| mean anomaly at epoch: | 278.7817° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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