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 60276U 26145.17899764 +.00000000 +00000-0 +30845-4 0 00007
2 60276 53.1602 56.8433 0001068 82.5599 277.5523 15.30196196 04
| Epoch (UTC): | 25 May 2026 04:17:45 |
| Eccentricity: | 0.0001068 |
| inclination: | 53.1602° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 56.8433° |
| argument of perigee: | 82.5599° |
| revolutions per day: | 15.30196196 |
| mean anomaly at epoch: | 277.5523° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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