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 62688U 26145.49745176 +.00000000 +00000-0 +26017-3 0 00003
2 62688 97.3981 228.6621 0002903 82.2228 277.9342 15.30326660 00
| Epoch (UTC): | 25 May 2026 11:56:19 |
| Eccentricity: | 0.0002903 |
| inclination: | 97.3981° |
| perigee height: | 473 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 228.6621° |
| argument of perigee: | 82.2228° |
| revolutions per day: | 15.30326660 |
| mean anomaly at epoch: | 277.9342° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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