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 53664U 26145.41778509 +.00000000 +00000-0 +13523-2 0 00002
2 53664 97.4512 26.4225 0001593 115.5928 244.5464 15.05564158 03
| Epoch (UTC): | 25 May 2026 10:01:36 |
| Eccentricity: | 0.0001593 |
| inclination: | 97.4512° |
| perigee height: | 549 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 26.4225° |
| argument of perigee: | 115.5928° |
| revolutions per day: | 15.05564158 |
| mean anomaly at epoch: | 244.5464° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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