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 64521U 26145.55171490 +.00000000 +00000-0 +49026-3 0 00005
2 64521 51.9004 248.2088 0000226 121.4259 238.6725 14.79856592 04
| Epoch (UTC): | 25 May 2026 13:14:28 |
| Eccentricity: | 0.0000226 |
| inclination: | 51.9004° |
| perigee height: | 630 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 248.2088° |
| argument of perigee: | 121.4259° |
| revolutions per day: | 14.79856592 |
| mean anomaly at epoch: | 238.6725° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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