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 63013U 26145.24896763 +.00000000 +00000-0 +20808-2 0 00009
2 63013 43.0003 93.9490 0001541 258.8655 101.2039 15.70914405 01
| Epoch (UTC): | 25 May 2026 05:58:30 |
| Eccentricity: | 0.0001541 |
| inclination: | 43.0003° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 93.9490° |
| argument of perigee: | 258.8655° |
| revolutions per day: | 15.70914405 |
| mean anomaly at epoch: | 101.2039° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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