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 64553U 26145.31067373 +.00000000 +00000-0 +14920-3 0 00003
2 64553 97.4717 261.0075 0002633 106.7061 253.4464 15.20767839 02
| Epoch (UTC): | 25 May 2026 07:27:22 |
| Eccentricity: | 0.0002633 |
| inclination: | 97.4717° |
| perigee height: | 502 km |
| apogee height: | 505 km |
| right ascension of ascending node: | 261.0075° |
| argument of perigee: | 106.7061° |
| revolutions per day: | 15.20767839 |
| mean anomaly at epoch: | 253.4464° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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