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 38077U 26145.57638639 +.00000000 +00000-0 -11852-4 0 00005
2 38077 69.4904 330.8680 0006731 53.5640 306.6006 12.54932082 04
| Epoch (UTC): | 25 May 2026 13:49:59 |
| Eccentricity: | 0.0006731 |
| inclination: | 69.4904° |
| perigee height: | 1439 km |
| apogee height: | 1449 km |
| right ascension of ascending node: | 330.8680° |
| argument of perigee: | 53.5640° |
| revolutions per day: | 12.54932082 |
| mean anomaly at epoch: | 306.6006° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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