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 49739U 26145.49796647 +.00000000 +00000-0 +10385-3 0 00005
2 49739 53.2121 174.3143 0001024 79.8128 280.2979 15.08833467 05
| Epoch (UTC): | 25 May 2026 11:57:04 |
| Eccentricity: | 0.0001024 |
| inclination: | 53.2121° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 174.3143° |
| argument of perigee: | 79.8128° |
| revolutions per day: | 15.08833467 |
| mean anomaly at epoch: | 280.2979° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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