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 63007U 26145.21180265 +.00000000 +00000-0 +14625-2 0 00002
2 63007 42.9998 93.6535 0001608 263.1575 96.9110 15.70849053 02
| Epoch (UTC): | 25 May 2026 05:04:59 |
| Eccentricity: | 0.0001608 |
| inclination: | 42.9998° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 93.6535° |
| argument of perigee: | 263.1575° |
| revolutions per day: | 15.70849053 |
| mean anomaly at epoch: | 96.9110° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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