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 60370U 26145.48637672 +.00000000 +00000-0 +32177-4 0 00004
2 60370 53.1617 313.0202 0000975 83.4889 276.6222 15.30206247 00
| Epoch (UTC): | 25 May 2026 11:40:22 |
| Eccentricity: | 0.0000975 |
| inclination: | 53.1617° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 313.0202° |
| argument of perigee: | 83.4889° |
| revolutions per day: | 15.30206247 |
| mean anomaly at epoch: | 276.6222° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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