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 60271U 26145.17277431 +.00000000 +00000-0 +58596-4 0 00006
2 60271 53.1610 57.5196 0001210 82.0084 278.1054 15.30198294 02
| Epoch (UTC): | 25 May 2026 04:08:47 |
| Eccentricity: | 0.0001210 |
| inclination: | 53.1610° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 57.5196° |
| argument of perigee: | 82.0084° |
| revolutions per day: | 15.30198294 |
| mean anomaly at epoch: | 278.1054° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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