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 62088U 26145.14653130 +.00000000 +00000-0 +17199-2 0 00007
2 62088 42.9997 302.5919 0000476 4.1587 355.9284 15.70858086 01
| Epoch (UTC): | 25 May 2026 03:31:00 |
| Eccentricity: | 0.0000476 |
| inclination: | 42.9997° |
| perigee height: | 356 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 302.5919° |
| argument of perigee: | 4.1587° |
| revolutions per day: | 15.70858086 |
| mean anomaly at epoch: | 355.9284° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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