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 62888U 26145.52230146 +.00000000 +00000-0 +13552-2 0 00004
2 62888 42.9998 78.0393 0002292 62.5890 297.5211 15.70877123 08
| Epoch (UTC): | 25 May 2026 12:32:06 |
| Eccentricity: | 0.0002292 |
| inclination: | 42.9998° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 78.0393° |
| argument of perigee: | 62.5890° |
| revolutions per day: | 15.70877123 |
| mean anomaly at epoch: | 297.5211° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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