▸Orbital parameters

Orbit class	SSO
Inclination	97.5415°
Eccentricity	0.0005767
Period	94.6 min
Apogee	503 km
Perigee	495 km
Mean motion	15.22186124 rev/day
RAAN	264.9086°
Arg of perigee	153.7994°
Mean anomaly	206.3534°
B*	3.0220e-4
Rev at epoch	15,122

▸Two-line element set (TLE)

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

1 58021U 23155F 26188.18678402 .00006870 00000-0 30220-3 0 9994

2 58021 97.5415 264.9086 0005767 153.7994 206.3534 15.22186124151223

▸ source OMM (JSON)

{
  "OBJECT_NAME": "CSC-2",
  "OBJECT_ID": "2023-155F",
  "EPOCH": "2026-07-07T04:28:58.139+00:00",
  "MEAN_MOTION": 15.22186124,
  "ECCENTRICITY": 0.0005767,
  "INCLINATION": 97.5415,
  "RA_OF_ASC_NODE": 264.9086,
  "ARG_OF_PERICENTER": 153.7994,
  "MEAN_ANOMALY": 206.3534,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 58021,
  "REV_AT_EPOCH": 15122,
  "BSTAR": 0.0003022,
  "MEAN_MOTION_DOT": 0.0000687,
  "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	CSC-2
Operator	Innovative Solutions In Space B.V.HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	Netherlands
Launch date	Oct 9, 2023HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	10HIGHvia 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/58021

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