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 60995U 26145.04388588 +.00000000 +00000-0 +69781-5 0 00000
2 60995 53.1600 265.1020 0001188 83.4296 276.6857 15.69713535 08
| Epoch (UTC): | 25 May 2026 01:03:11 |
| Eccentricity: | 0.0001188 |
| inclination: | 53.1600° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 265.1020° |
| argument of perigee: | 83.4296° |
| revolutions per day: | 15.69713535 |
| mean anomaly at epoch: | 276.6857° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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