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 63949U 26145.24584191 +.00000000 +00000-0 +50503-3 0 00002
2 63949 70.0010 81.2657 0003001 264.8714 95.2102 14.98339974 02
| Epoch (UTC): | 25 May 2026 05:54:00 |
| Eccentricity: | 0.0003001 |
| inclination: | 70.0010° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 81.2657° |
| argument of perigee: | 264.8714° |
| revolutions per day: | 14.98339974 |
| mean anomaly at epoch: | 95.2102° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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