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 63180U 26145.47813066 +.00000000 +00000-0 +77389-4 0 00002
2 63180 97.9545 330.9385 0008836 237.3669 122.6688 14.74320885 06
| Epoch (UTC): | 25 May 2026 11:28:30 |
| Eccentricity: | 0.0008836 |
| inclination: | 97.9545° |
| perigee height: | 641 km |
| apogee height: | 654 km |
| right ascension of ascending node: | 330.9385° |
| argument of perigee: | 237.3669° |
| revolutions per day: | 14.74320885 |
| mean anomaly at epoch: | 122.6688° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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