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 64874U 26145.53246801 +.00000000 +00000-0 +13504-3 0 00005
2 64874 97.3975 210.9694 0003263 36.4182 323.7275 15.20295810 02
| Epoch (UTC): | 25 May 2026 12:46:45 |
| Eccentricity: | 0.0003263 |
| inclination: | 97.3975° |
| perigee height: | 503 km |
| apogee height: | 507 km |
| right ascension of ascending node: | 210.9694° |
| argument of perigee: | 36.4182° |
| revolutions per day: | 15.20295810 |
| mean anomaly at epoch: | 323.7275° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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