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 63298U 26145.64322421 +.00000000 +00000-0 +11957-2 0 00008
2 63298 97.6488 291.2488 0007444 211.8951 148.1842 15.36461978 00
| Epoch (UTC): | 25 May 2026 15:26:14 |
| Eccentricity: | 0.0007444 |
| inclination: | 97.6488° |
| perigee height: | 451 km |
| apogee height: | 462 km |
| right ascension of ascending node: | 291.2488° |
| argument of perigee: | 211.8951° |
| revolutions per day: | 15.36461978 |
| mean anomaly at epoch: | 148.1842° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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