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 63932U 26145.22917176 +.00000000 +00000-0 +27294-3 0 00006
2 63932 70.0010 81.6254 0003339 268.4658 91.6118 14.98337545 01
| Epoch (UTC): | 25 May 2026 05:30:00 |
| Eccentricity: | 0.0003339 |
| inclination: | 70.0010° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 81.6254° |
| argument of perigee: | 268.4658° |
| revolutions per day: | 14.98337545 |
| mean anomaly at epoch: | 91.6118° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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