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 60384U 26145.60326630 +.00000000 +00000-0 +10141-3 0 00008
2 60384 88.9720 282.0259 0015083 85.5398 274.7476 13.51009081 05
| Epoch (UTC): | 25 May 2026 14:28:42 |
| Eccentricity: | 0.0015083 |
| inclination: | 88.9720° |
| perigee height: | 1057 km |
| apogee height: | 1080 km |
| right ascension of ascending node: | 282.0259° |
| argument of perigee: | 85.5398° |
| revolutions per day: | 13.51009081 |
| mean anomaly at epoch: | 274.7476° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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