▸Orbital parameters

Orbit class	SSO
Inclination	97.7651°
Eccentricity	0.0000471
Period	96.5 min
Apogee	592 km
Perigee	591 km
Mean motion	14.92007264 rev/day
RAAN	146.8789°
Arg of perigee	295.2779°
Mean anomaly	3.0280°
B*	-5.4629e-3
Rev at epoch	545

▸Two-line element set (TLE)

EPOCH Jul 7, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 68484U 26067BW 26188.08336806 -.00054973 00000-0 -54629-2 0 9998

2 68484 97.7651 146.8789 0000471 295.2779 3.0280 14.92007264 5455

▸ source OMM (JSON)

{
  "OBJECT_NAME": "VINDLER 2.2",
  "OBJECT_ID": "2026-067BW",
  "EPOCH": "2026-07-07T02:00:03+00:00",
  "MEAN_MOTION": 14.92007264,
  "ECCENTRICITY": 0.0000471,
  "INCLINATION": 97.7651,
  "RA_OF_ASC_NODE": 146.8789,
  "ARG_OF_PERICENTER": 295.2779,
  "MEAN_ANOMALY": 3.028,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 68484,
  "REV_AT_EPOCH": 545,
  "BSTAR": -0.0054629,
  "MEAN_MOTION_DOT": -0.00054973,
  "MEAN_MOTION_DDOT": 0
}

Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.

▸Satellite metadata

Name	VINDLER 2.2
Operator	Sierra Nevada Corp.HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Mar 30, 2026HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	130HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/68484

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.