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 57217U 26145.59518652 +.00000000 +00000-0 +41915-3 0 00007
2 57217 97.5078 209.8536 0011665 168.7790 191.3712 15.29254091 02
| Epoch (UTC): | 25 May 2026 14:17:04 |
| Eccentricity: | 0.0011665 |
| inclination: | 97.5078° |
| perigee height: | 470 km |
| apogee height: | 486 km |
| right ascension of ascending node: | 209.8536° |
| argument of perigee: | 168.7790° |
| revolutions per day: | 15.29254091 |
| mean anomaly at epoch: | 191.3712° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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