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 49770U 26145.44188812 +.00000000 +00000-0 +11145-3 0 00009
2 49770 53.2111 154.6159 0001013 68.0438 292.0661 15.08833855 09
| Epoch (UTC): | 25 May 2026 10:36:19 |
| Eccentricity: | 0.0001013 |
| inclination: | 53.2111° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 154.6159° |
| argument of perigee: | 68.0438° |
| revolutions per day: | 15.08833855 |
| mean anomaly at epoch: | 292.0661° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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