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 60029U 26145.10900053 +.00000000 +00000-0 +13352-4 0 00004
2 60029 53.1600 80.6647 0001256 86.6857 273.4288 15.30197495 07
| Epoch (UTC): | 25 May 2026 02:36:57 |
| Eccentricity: | 0.0001256 |
| inclination: | 53.1600° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 80.6647° |
| argument of perigee: | 86.6857° |
| revolutions per day: | 15.30197495 |
| mean anomaly at epoch: | 273.4288° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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