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 60937U 26145.27201910 +.00000000 +00000-0 +49748-4 0 00004
2 60937 53.1594 134.1167 0001469 82.6057 277.5110 15.30195104 07
| Epoch (UTC): | 25 May 2026 06:31:42 |
| Eccentricity: | 0.0001469 |
| inclination: | 53.1594° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 134.1167° |
| argument of perigee: | 82.6057° |
| revolutions per day: | 15.30195104 |
| mean anomaly at epoch: | 277.5110° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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