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 data is extracted from the following two-line orbital elements,
1 28888U 05042A 25139.08827680 0.00035000 00000-0 25027-3 0 04
2 28888 97.0197 182.7394 0015730 30.2901 329.7098 15.73539132 01
| Epoch (UTC): | 19 May 2025 02:07:07 |
| Eccentricity: | 0.0015730 |
| inclination: | 97.0197° |
| perigee height: | 338 km |
| apogee height: | 359 km |
| right ascension of ascending node: | 182.7394° |
| argument of perigee: | 30.2901° |
| revolutions per day: | 15.73539132 |
| mean anomaly at epoch: | 329.7098° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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