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 49760U 26145.40780972 +.00000000 +00000-0 +23550-4 0 00003
2 49760 53.2111 154.7161 0001116 59.1559 300.9543 15.08838217 06
| Epoch (UTC): | 25 May 2026 09:47:14 |
| Eccentricity: | 0.0001116 |
| inclination: | 53.2111° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 154.7161° |
| argument of perigee: | 59.1559° |
| revolutions per day: | 15.08838217 |
| mean anomaly at epoch: | 300.9543° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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