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 63195U 26145.61033767 +.00000000 +00000-0 +11615-2 0 00004
2 63195 43.0003 216.7021 0001535 264.2897 95.7795 15.70840751 07
| Epoch (UTC): | 25 May 2026 14:38:53 |
| Eccentricity: | 0.0001535 |
| inclination: | 43.0003° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 216.7021° |
| argument of perigee: | 264.2897° |
| revolutions per day: | 15.70840751 |
| mean anomaly at epoch: | 95.7795° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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