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 57203U 26145.58836402 +.00000000 +00000-0 +41212-3 0 00007
2 57203 97.5099 212.5057 0009167 151.3289 208.8458 15.31404967 07
| Epoch (UTC): | 25 May 2026 14:07:14 |
| Eccentricity: | 0.0009167 |
| inclination: | 97.5099° |
| perigee height: | 465 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 212.5057° |
| argument of perigee: | 151.3289° |
| revolutions per day: | 15.31404967 |
| mean anomaly at epoch: | 208.8458° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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