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 49769U 26145.43451867 +.00000000 +00000-0 +10802-3 0 00008
2 49769 53.2138 154.6490 0001040 65.8597 294.2504 15.08853769 01
| Epoch (UTC): | 25 May 2026 10:25:42 |
| Eccentricity: | 0.0001040 |
| inclination: | 53.2138° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 154.6490° |
| argument of perigee: | 65.8597° |
| revolutions per day: | 15.08853769 |
| mean anomaly at epoch: | 294.2504° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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