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 60137U 26145.49797137 +.00000000 +00000-0 +15905-4 0 00009
2 60137 53.1613 323.3189 0001152 80.3685 279.7448 15.34391172 03
| Epoch (UTC): | 25 May 2026 11:57:04 |
| Eccentricity: | 0.0001152 |
| inclination: | 53.1613° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 323.3189° |
| argument of perigee: | 80.3685° |
| revolutions per day: | 15.34391172 |
| mean anomaly at epoch: | 279.7448° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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