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 62887U 26145.53731557 +.00000000 +00000-0 +17553-2 0 00001
2 62887 42.9993 78.1611 0001021 82.9516 277.1468 15.70886255 00
| Epoch (UTC): | 25 May 2026 12:53:44 |
| Eccentricity: | 0.0001021 |
| inclination: | 42.9993° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 78.1611° |
| argument of perigee: | 82.9516° |
| revolutions per day: | 15.70886255 |
| mean anomaly at epoch: | 277.1468° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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