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 49763U 26145.47036823 +.00000000 +00000-0 -85438-4 0 00006
2 49763 53.2115 154.4382 0001264 75.8687 284.2446 15.08845486 08
| Epoch (UTC): | 25 May 2026 11:17:19 |
| Eccentricity: | 0.0001264 |
| inclination: | 53.2115° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 154.4382° |
| argument of perigee: | 75.8687° |
| revolutions per day: | 15.08845486 |
| mean anomaly at epoch: | 284.2446° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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