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 28097U 03054C 23267.81937831 0.00000400 00000-0 34014-3 0 00
2 28097 63.4008 223.2943 0505140 2.5046 357.4954 13.40889117 05
| Epoch (UTC): | 24 September 2023 19:39:54 |
| Eccentricity: | 0.0505140 |
| inclination: | 63.4008° |
| perigee height: | 728 km |
| apogee height: | 1484 km |
| right ascension of ascending node: | 223.2943° |
| argument of perigee: | 2.5046° |
| revolutions per day: | 13.40889117 |
| mean anomaly at epoch: | 357.4954° |
| 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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