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 57671U 26145.56195315 +.00000000 +00000-0 +64617-5 0 00001
2 57671 53.1606 209.9496 0001141 93.4112 266.7019 15.30188601 09
| Epoch (UTC): | 25 May 2026 13:29:12 |
| Eccentricity: | 0.0001141 |
| inclination: | 53.1606° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 209.9496° |
| argument of perigee: | 93.4112° |
| revolutions per day: | 15.30188601 |
| mean anomaly at epoch: | 266.7019° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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