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 64858U 26145.32738684 +.00000000 +00000-0 +21905-3 0 00003
2 64858 97.4494 0.7220 0002517 84.7123 275.4391 15.05658570 04
| Epoch (UTC): | 25 May 2026 07:51:26 |
| Eccentricity: | 0.0002517 |
| inclination: | 97.4494° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 0.7220° |
| argument of perigee: | 84.7123° |
| revolutions per day: | 15.05658570 |
| mean anomaly at epoch: | 275.4391° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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