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 55137U 26145.65311170 +.00000000 +00000-0 +30657-3 0 00000
2 55137 97.1443 221.1247 0004414 172.5725 187.5595 15.54083472 01
| Epoch (UTC): | 25 May 2026 15:40:28 |
| Eccentricity: | 0.0004414 |
| inclination: | 97.1443° |
| perigee height: | 402 km |
| apogee height: | 408 km |
| right ascension of ascending node: | 221.1247° |
| argument of perigee: | 172.5725° |
| revolutions per day: | 15.54083472 |
| mean anomaly at epoch: | 187.5595° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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