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 38995U 26135.71280542 +.00000000 +00000-0 +00000-0 0 00003
2 38995 64.1352 359.9560 7339753 228.5544 40.2800 2.00653594 09
| Epoch (UTC): | 15 May 2026 17:06:26 |
| Eccentricity: | 0.7339753 |
| inclination: | 64.1352° |
| perigee height: | 685 km |
| apogee height: | 39663 km |
| right ascension of ascending node: | 359.9560° |
| argument of perigee: | 228.5544° |
| revolutions per day: | 2.00653594 |
| mean anomaly at epoch: | 40.2800° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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