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 64951U 26145.14798896 +.00000000 +00000-0 +37675-3 0 00009
2 64951 97.4490 9.1180 0002665 78.9010 281.2517 15.05661684 01
| Epoch (UTC): | 25 May 2026 03:33:06 |
| Eccentricity: | 0.0002665 |
| inclination: | 97.4490° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 9.1180° |
| argument of perigee: | 78.9010° |
| revolutions per day: | 15.05661684 |
| mean anomaly at epoch: | 281.2517° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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