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 51769U 26145.31131095 +.00000000 +00000-0 +49468-3 0 00006
2 51769 53.2172 355.0659 0001493 96.5318 263.5844 15.09441439 04
| Epoch (UTC): | 25 May 2026 07:28:17 |
| Eccentricity: | 0.0001493 |
| inclination: | 53.2172° |
| perigee height: | 537 km |
| apogee height: | 539 km |
| right ascension of ascending node: | 355.0659° |
| argument of perigee: | 96.5318° |
| revolutions per day: | 15.09441439 |
| mean anomaly at epoch: | 263.5844° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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