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 62844U 26145.62250337 +.00000000 +00000-0 +37576-3 0 00004
2 62844 43.0002 14.7776 0000513 57.0269 303.0632 15.27600913 06
| Epoch (UTC): | 25 May 2026 14:56:24 |
| Eccentricity: | 0.0000513 |
| inclination: | 43.0002° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 14.7776° |
| argument of perigee: | 57.0269° |
| revolutions per day: | 15.27600913 |
| mean anomaly at epoch: | 303.0632° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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