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 63008U 26145.13333110 +.00000000 +00000-0 +12004-2 0 00002
2 63008 43.0023 94.8104 0001895 263.2275 96.8377 15.70863977 00
| Epoch (UTC): | 25 May 2026 03:11:59 |
| Eccentricity: | 0.0001895 |
| inclination: | 43.0023° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 94.8104° |
| argument of perigee: | 263.2275° |
| revolutions per day: | 15.70863977 |
| mean anomaly at epoch: | 96.8377° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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